PKK Library Search for 'pb:NACA'

MEASUREMENT OF THE HANDLING CHARACTERISTICS OF TWO LIGHT AIRPLANES

Naca, Washington 1980 . 77

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VALIDATION OF A FLEXIABLE AIRCRAFT TAKE-OFF AND LANDING ANALYSIS(FATOLA)

By Carden,Huey D,Mcgehee,John R. Naca,Washington 1977 . 66

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REAL-TIME FLIGHT TEST DATA DISTRIBUTION AND DISPLAY

By Nesel,Michael C.. Naca, Washington 1988

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DRAG OF CIRCULAR CYLINDERS FOR A WIDE RANGE OF REYNOLDS MEMBERS AND MACH NUMBERS

By Gowen,Forrest E.. Naca, Washington 1963 . 26 , Bound With: Naca-Tn.No.2960

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PRELIMINARY EXPERIMENTAL INVESTIGATION OF LOW-SPEED TURBULENT BOUNDARY LAYERS IN ADVERSE PRESSURE GRADIENTS

By Sandborn,Virgil A.. Naca, Washington 1953 . 37 , Bound With: Naca-Tn-3031-3040

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AN ANALYTICAL STUDY OF THE EFFECT OF AIRPLANE WAKE ON THE LATERAL DISPERSION OF AERIAL SPRAYS

By Reed,Wilmes H.. Naca, Washington 1953 . 46 , Bound With: Naca-Tn-3031-3040

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APPLICATION OF AN ELECTRO-OPTICAL TWO-COLOR PYROMETER TO MEASUREMENT OF FLAME TEMPERATURE FOR LIQUID OXYGEN-HYDROCARBON PROPELLANT COMBINATION

By Heidmann,M. F.. Naca, Washington 1953 . 39 , Bound With: Naca-Tn-3031-3040

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GRAPHICAL SOLUTION OF SOME AUTOMATIC-CONTROL PROBLEMS INVOLVING SATURATION EFFECTS WITH APPLICATION TO YAW DAMPERS FOR AIRCRAFT

By Phillips,William H.. Naca, Washington 1953 . 42 , Bound With: Naca-Tn 3031-3040

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A PRCLIMINARY STUDY OF THE PROBLEM OF DESIGNING HIGH-SPEED AIRPLANES WITH SATISFACTORY INHERENT DAMPING OF THE DUTCH SOLL OSCILLATION

By Campbell,John P.. Naca, Washington 1953 . 40 , Bound With: Naca-Tn-3031-3040

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THE FLOW ABOUT A SECTION OF A FINITE-ASPECT-RATIO NACA 0015 AIRFOIL ON A TRANSONIC BUMP

By Mellenthin,Jack A.. Naca, Washington 1953 . 30 , Bound With: Naca-Tn-3031-3040

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LOW-SPEED DRAG OF CYLINDERS OF VARIOUS SHAPES

By Delany,Noel K.. Naca, Washington 1953 . 22 , Bound With: Naca-Tn-3031-3040

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EXPERIMENTAL STRESS ANALYSIS OF STIFFENED CYLINDERS WITH COTOUTS

By Schlechte,Floyd R.. Naca, Washington 1953 . 41 , Bound With: Naca-Tn-3031-3040

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USE OF TWO-DIMENSIONAL DATA IN ESTIMATING LOADS ON A 45 % SWEPTBACK WIND WITH SLATS AND PARTIAL -SPAN FLAPS

By Hunton,Lynn W.. Naca, Washington 1953 . 40 , Bound With: Naca-Tn-3031-3040

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SOME MEASUREMENTS OF FLOW IN A RECTANGULAR CUTOUT

By Roshko,Anatol. Naca, Washington 1955 . 21 , Bound With Naca Tn 3480-87,3489

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CONTRIBUTIONS ON THE MECHANICS OF BOUNDARY-LAYER TRANSITION

By Schubauer,G B. Naca, Washington 1955 . 31 , Bound With Naca Tn 3480-88

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FREE-SPINNING-TUNNEL INVESTIGATION OF GYROSCOPIC EFFECTS OF JET-ENGINE ROTATING PARTS (OR OF ROTATING PROPELLERS) ON SPIN AND SPIN RECOVERY

By Bowman,James S. Naca, Washington 1955 . 21 , Bound With Naca Tn 3481-89

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HANDBOOK OF STRUCTURAL STABILITY

By Gerald,G,Becker,H. Naca,Washington 1957 . 102 , Bound With Naca Tn 3780,82-3789.

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HANDBOOK OF STRUCTURAL STABILITY

By Becker,H. Naca,Washington 1957 . 72 , Bound With Naca Tn 3780-81, 3783-89.

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HANDBOOK OF STRUCTURAL STABILITY

By Gerard,G,Becker,H. Naca,Washington 1957 . 154 , Bound With Naca Tn 3780-82, 3784-89.

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HANDBOOK OF STRUCTURAL STABILITY

By Gerard,G. Naca,Washington 1957 . 93 , Bound With Naca Tn 3780-83, 3785-89.

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IMPINGMENT OF WATER DROPLETS ON AN ELLIPSOID ITH FINESS RATIO 5 IN AXISMMETRIC FLOW.

By Dorsch,Robert G,Brun,Rinaldo J. Naca, Washington 1954 . 50 , Bound With Naca Tn -3090-98.

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INVESTIGATION OF SANDWICH CONSTRUCTION UNDER LATERAL AND AXIAL LOADS

By Kroll,Wilhelmina D,Mordfin,Leonard. Naca, Washington 1953 . 58 , Bound With Naca Tn 3091-99

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HANDBOOK OF STRUCTURAL STABILITY

By Gerard,G. Naca, Washington 1957 . 89 , Bound With Naca Tn 3780-84, 3786-89.

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HANDBOOK OF STRUCTURAL STABILITY

By Becker,H. Naca, Washington 1958 . 82 , Bound With Naca Tn 3780-85, 3787-89.

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HEAT-CAPACITY MEASUREMENTS OF TITANIUM AND OF A HYDRIDE OF TITANIUM FOR TEMPERATURES FROM 4 DEGREE TO 15 DEGREE K INCLUDING A DETAILED DESCRIPTION OF A SPECIAL ADIABATIC SPECIFIC-HEAT CALORIMETER

By Aven,M H,Craig,R S. Naca, Washington 1956 . 30 , Bound With Naca Tn 3780-86, 3788-89.

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STABILITY DERIVATIVES OF CONES AT SUPERSONIC SPEEDS

By Tobak,M. Naca, Washington 1956 . 43 , Bound With Naca Tn 3780-87, 3789.

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THE RESULTS OF WIND-TUNNEL TESTS TO A MACH NUMBER OF 0.90 OF A FOUR-ENGINE PROPELLER-DRIVEN AIRPLANE CONFIGURATION HAVING A WING WITH 40 DEGREE OF SWEEPBACK AND AN ASPECT RATIO OF 10

By Edwards,G G,Dickson,J K. Naca, Washington 1956 . 171 , Bound With Naca Tn 3780-88.

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AT LOW SPEED OF EFFECT OF SIZE AND POSITION OF CLOSED AIR DUCTS ON STATIC LONGITUDINAL AND STATIC LATERAL STABILITY CHARACTERISTICS OF UNSWEPT-MIDWING MODELS HAVING WINGS OF ASPECT RATIO 2,4, AND 6

By Jaquet,Byron M. Naca, Washington 1955 . 45 , Bound With Naca Tn 3480,3482-89

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SUPPLEMENTARY CHARTS FOR ESTIMATING PERFORMANCE OF HIGH-PERFORMANCE HELICOPTERS

By Tapscott,Robert J. Naca, Washington 1955 . 31 , Bound With Naca Tn 3480-81,3483-89

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AN ANALYSIS OF ACCELERATION, AIRSPEED, AND GUST-VELOCITY DATA FROM A FOUR-ENGINE TRANSPORT AIRPLANE IN OPERATIONS ON AN EASTERN UNITED STATES ROUTE

By Coleman,Thomas L. Naca, Washington 1955 . 20 , Bound With Naca Tn 3480-82,3484-89

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ON SPECTRAL ANALYSIS OF RUNWAY ROUGHNESS AND LOADS DEVELOPED DURING TAXIING

By Houbolt,John C,Walls,James H. Naca, Washington 1955 . 9 , Bound With Naca Tn 3480-83,3485-89

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AN APPROXIMATE SOLUTION FOR AXIALLY SYMMETRIC FLOW OVER A CONE WITH AN ATTACHED SHOCK WAVE

By Hord,Richard A. Naca, Washington 1955 . 32 , Bound With Naca Tn 3480-84,3486-89

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MEASUREMENTS OF TURBULENT SKIN FRICTION ON A FLAT PLATE AT TRANSONIC SPEEDS

By Hakkinen,Raimo J. Naca, Washington 1955 . 41 , Bound With Naca Tn 3480-85,3487-89

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ACOUSTIC RADIATION FROM TWO-DIMENSIONAL RECTANGULAR CUTOUTS IN AERODYNAMIC SURFACES

By Krishnamurty,K. Naca, Washington 1955 . 33 , Bound With Naca Tn 3480-86,3488-89

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EFFECT OF CHEMICAL REACTIVITY OF LUBRICANT ADDITIVES ON FRICTION AND SURFACE WELDING AT HIGH SLIDING VELOCITIES

By Bisson,E E,Swikert,M A. Naca, Washington 1950 . 33 , Bound With Naca Tn-2140-43, 2145-49.

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LIFT-CANCELLATION TECHNIQUE IN LINEARIZED SUPERSONIC-WING THEORY

By Mirels,H. Naca, Washington 1950 . 43 , Bound With Naca Tn-2140-44, 2146-49.

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ON THE EFFECT OF SUBSONIC TRAILING EDGES ON DAMPING IN ROLL AND PITCH OF THIN SWEPTBACK WINGS IN A SUPERSONIC STREAM

By Ribner,H S. Naca, Washington 1950 . 27 , Bound With Naca Tn-2140-45, 2147-49.

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SOME CONICAL AND QUASI-CONICAL FLOWS IN LINEARIZED SUPERSONIC-WING THEORY

By Ribner,H S. Naca, Washington 1950 . 61 , Bound With Naca Tn-2140-46, 2148-49.

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INVESTIGATION OF BOUNDARY-LAYER CONTROL TO IMPROVE THE LIFT AND DRAG CHARACTERISTICS OF THE NACA 652-415 AIRFOIL SECTION WITH DOUBLE SLOTTED AND PLAIN FLAPS

By Horton,E A,Racisz,S F. Naca, Washington 1950 . 63 , Bound With Naca Tn-2140-48.

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THEORETICAL ANTISYMMETRIC SPAN LOADING FOR WINGS OF ARBITRARY PLAN FORM AT SUBSONIC SPEEDS

By Young,J D. Naca, Washington 1950 . 95 , Bound With Naca Tn-2141-49.

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CHARTS FOR ESTIMATING DOWNWASH BEHIND RECTANGULAR TRAPEZOIDAL AND TRIANGULAR WING AT SUPERSONIC SPEEDS

By Haefeli,R C,Mirerls,H. Naca, Washington 1950 . 67 , Bound With Naca Tn-2140, 42-2149.

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PHOTOMICROGRAPHIC INVESTIGATION OF SPONTANEOUS FREEZING TEMPERATURES OF SUPERCOLD WATER DROPLETS

By Dorsch,R G. Naca, Washington 1950 . 57 , Bound With Naca Tn-2140-41, 2143-49.

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ANALYSIS OF THE EFFECTS OF BOUNDARY-LAYER CONTROL ON THE POWER-OFF LANDING PERFORMANCE CHARACTERISTICS OF A LIALSON TYPE OF AIRPLANE

By Horton,E A,Loftin,L K. Naca, Washington 1950 . 51 , Bound With Naca Tn-2140-42, 2144-49.

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FLOW PROPERTIES OF STRONG SHOCK WAVES IN XENON GAS AS DETERMINED FOR THERMAL EQUILIBRIUM CONDITIONS

By Sabol,Alexander P. Naca, Washington 1953 . 29 , Bound With Naca Tn 3090,3092-99

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HYDRODYNAMIC DRAG OF 12-AND 21- PERCENT-THICK SUFACE-PIERING STRUTS.

By Coffee,Claude W. Naca, Washington 1953 . 28 , Bound With Naca Tn-3091,3093-3099.

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EFFECT OF TYPE OF POROUS SURFACE AND SUCTION VELOCITY DISTRIBUTION ON THE CHARACTERISTICS OF.A 10.5-PERCENT-THICK AIRFOIL WITH AREA SUCTION.

By Dannerberg,Robert E,Weiberg,James A. Naca,Washington 1953 . 59 , Bound With Naca Tn-3090-92,3094-99.

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THE RESISTANCE TO AIR FLOW OF POROUS MATERIALS SUITABLE FOR BOUNDARY-LAYER-CONTROL APPLICATIONS USING AREA SUCTION.

By Dannenberg,Robert E,Weiberg,James A. Naca, Washington 1954 . 21 , Bound Wit Naca Tn-3090-3093,3095-99.

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THE AMES 10-BY 14-INCH SUPRESONIC WIND TUNNEL.

By Eggers,A J. Naca, Washington 1954 . 43 , Bound With Naca Tn-3090-94,3096-99.

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THEORITICAL PREDICATION OF PRESSURE DISTRIBUTIONS ON NONLIFTING AIRFOILS AT HIGH SUBSONIC SPEEDS.

By Spreiter,John R. Naca, Washington 1954 . 84 , Bound With Naca Tn- 3090-95,3097-3099.

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TURBULENT BOUNDARY-LAYERS AND SKIN-FRICTION MEASUREMENTS IN AXIAL FLOW ALONG CYLINDERS AT MACH NUMBERS BETWEEN 0.5 AND 3.6.

By Chapman,Dean R,Kester,Robert H. Naca,Washington 1954 . 53 , Bound With Naca Tn-3090-96,3098-99.

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DENSITY PROFILES OF SUBSONIC BOUNDARY LAYERS ON A FLAT PLATE DETERMINED BY X-RAY AND PRESSURE MEASUREMENTS.

By Weltmann,Ruth N. Naca, Washington 1954 . 29 , Bound With Naca Tn-3090-97,3099.

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WING-FUSELAGE INTERFERENCE TAIL BUFFETING, AND FLOW ABOUT THE TAIL OF A LOW-WING MONOPLANE.

By White,James A. Naca, Washington 1934 . 21 , Bound With Naca-481,483-500

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EFFECT OF MODERATE AIR FLOW ON THE DISTRIBUTION OF FUEL SPRAYS AFTER INJECTION CUT-OFF.

By Rothrock,A M. Naca, Washington 1934 . 10 , Bound With Naca-481-482,484-500.

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A FLIGHT INVESTIGATION OF THE EFFECT OF MASS DISTRIBUTION AND CONTROL SETTING ON THE SPINNING OF THE XN2Y-1 AIRPLANE.

By Scudder,N F. Naca, Washington 1934 . 9 , Bound With Naca -481-483,485-500.

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AN AERODYNAMIC ANALYSIS OF THE AUTOGIRD ROTOR WITH A COMPARISON BETWEEN CALCULATED AND EXPERMENTAL RESULTS.

By Wheatley,John B. Naca, Washington 1934 . 17 , Bound With Naca-481-486,488-500.

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HEAT TRANSFER FROM FINNED METAL CYLINDERS IN AN AIR STREAM.

By Biermann,Arnold E. Naca, Washington 1934 . 20 , Bound With Naca-481-487,489-500.

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AIR CONDITIONS CLOSE TO THE GROUND AND THE EFFECT ON AIRPLANE LANDINGS.

By Thomson,F L,Peck,W C. Naca, Washington 1934 . 35 , Bound With Naca-481-488,490-500.

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VIBRATIONS RESPONSE OF AIRPLANE STRUCTURES.

By Theodorsen,T. Naca, Washington 1934 . 22 , Bound With Naca-481-490,492-500.

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TESTS OF A 16 RELATED AIRFOILS AT HIGH SPEEDS.

By Stack,John. Naca, Washington 1934 . 23 , Bond With Naca-481-491,493-500.

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THE PHYSICAL EFFECTS OF DETONATION IN A CLOSED CYLINDRICAL CHAMBER.

By Draper,C S. Naca, Washington 1934 . 16 , Bound With Naca-481-492,494,495-500.

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GENERAL THEORY OF AERODYNAMIC INSTABILITY AND THE MECHANISM OF FLUTTER.

By Theodorsen,Theodore. Naca, Washington 1935 . 17 , Bound With Naca-481-495,497-500.

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COMPUTATION OF THE TWO-DIMENSIONAL, FLOW IN A LAMINAR BOUNDARY LAYER.

By Dryden,Hugh L. Naca, Washington 1934 . 11 , Bound With Naca-481-496,498-500.

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IMPROVED AIRPLANE WINDSHIELDS TO PROVIDE VISION IN STORARY WEATHER

By Clay,William C. Naca, Washington 1934 . 19 , Bound With Naca- 481-497,499-500.

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WIND-TUNNEL RESEARCH COMPARING LATERAL CONTROL DEVICES,PARATICULARY AT HIGH ANGLES OF ATTACK.

By Weick,Fred E. Naca, Washington 1934 . 17 , Bound With Naca-481-498,500.

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INFRARED RADIATION FROM EXPOLSIONS IN A SPARK-IGNATION ENGINE.

By Marvin,Chrales F,Caldwell,Frack R. Naca, Washington 1934 . 486 , Bound With Naca-481-485,487-500

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DISCUSSION OF PROBLEMS RELATING TO THE SAFETY OF AVIATION.

By Sabtier,J. Naca,Washington 1928 . 32 , Bound With Naca Tm-455,470.

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ON IMPROVEMENT OF AIR FLOW IN WIND TUNNELS .

By Wieselsberger,C. Naca, Washington 1928 . 40 , Bpund With Naca Tm-455,465.

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EXPERIMENTAL INVESTIGATION AT LOW SPEED OF EFFECTS OF FUSELAGE CROSS SECTION ON STATIC LONGITUDINAL AND LATERAL STABILITY CHARACTERISTICS OF MODELS HAVING 0(DEGRE) AND 45(DEGRE) SWEPTBACK SURFACES

By Letko,William. Naca, Washington 1955 . 45 , Bound With Naca Tn 3550,3552-3559

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INVESTIGATION OF THE COMPRESSIVE STRENGTH AND CREEP LIFETIME OF 2024-T3 ALUMINUM-ALLOY PLATES AT ELEVATED TEMPERATURES 1

By Mathauser,Eldon E. Naca, Washington 1955 . 31 , Bound With Naca Tn 3550-3551,3553-3559

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COMPRESSIVE CRIPPLING OF STRUCTURAL SECTIONS

By Anderson,Melvin S. Naca, Washington 1955 . 31 , Bound With Naca Tn 3550-3552,3554-3559

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A PRELIMINARY INVESTIGATION OF THE EFFECTS OF FREQUENCY AND AMPLITUDE ON THE ROLLING DERIVATIVES OF AN UNSWEPT-WING MODEL OSCILLATING IN ROLL

By Fisher,Lewis R,Lichtenstein,Jacob H. Naca, Washington 1955 . 29 , Bound With Naca Tn 3550-3553,3555-3559

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A METHOD FOR CALCULATING THE CONTOUR OF BODIES OF REVOLUTION WITH A PRESCRIBED PRESSURE GRADIENT AT SUPERSONIC SPEED WITH EXPERIMENTAL VERIFICATION

By Burbank,Paige B. Naca, Washington 1955 . 64 , Bound With Naca Tn 3550-3554,3556-3559

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GRAIN-BOUNDARY BEHAVIOR IN CREEP OF ALUMINUM BICRYSTALS

By Rhines,F N,Bond,W E. Naca, Washington 1955 . 56 , Bound With Naca Tn 3550-3555,3557-3559

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A THEORETICAL ANALYSIS OF THE FIELD OF A RANDOM NOISE SOURCE ABOVE AN INFINITE PLANE

By Franken,Peter A. Naca, Washington 1955 . 20 , Bound With Naca Tn 3550-3556,3558-3559

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HEAT CAPACITY LAG OF GASEOUS MIXTURES

By Rossing,Thomas D,Amme,Robert C. Naca, Washington 1955 . 35 , Bound With Naca Tn 3550-3557,3559

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LAMINAR SEPARATION OVER A TRANSPIRATION-COOLED SURFACE IN COMPRESSIBLE FLOW

By Morduchow,Morris. Naca, Washington 1955 . 32 , Bound With Naca Tn 3550-3558

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ON THE KERNEL FUNCTION OF THE INTGERAL EQUATION RELATING THE LIFT AND DOWNWASH DISTRIBUTIONS OF OSCIL

By Watkins,Charles E,Runyan,Harry L. Naca, Washington 1954 . 44 , Bound With Naca Tn-3130,3132-3139.

Place Hold on ON THE KERNEL FUNCTION OF THE INTGERAL EQUATION RELATING THE LIFT AND DOWNWASH DISTRIBUTIONS OF OSCIL

TAIGIE TESTS AT STRESSES PRODUCING FAILIURE IN 2 TO 10.000 CYCLES.

By Hardrath,Herbert. Naca, Washington 1954 . 14 , Bound With Naca Tn-3130-3131,3133-3139.

Place Hold on TAIGIE TESTS AT STRESSES PRODUCING FAILIURE IN 2 TO 10.000 CYCLES.

THE FREE-STREAM BOUNDARIES OF TUBULENT FLOWS.

By Corrsin,Stanley. Naca, Washington 1954 . 109 , Bound With Naca Tn-3130-3132,3134-3139.

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A METHOD FOR ESTIMATING VARIATIONS TN THE ROOTS OF THE LATERAL-STABILITY QUARTIC DUE TO CHANGES IN MASS AND AERODYNAMIC OPARAMETERS OF AN AIRPLANE.

By Gates,Ordway B. Naca, Washington 1954 . 66 , Bound With Naca Tn-3130-3133,3135-3139.

Place Hold on A METHOD FOR ESTIMATING VARIATIONS TN THE ROOTS OF THE LATERAL-STABILITY QUARTIC DUE TO CHANGES IN MASS AND AERODYNAMIC OPARAMETERS OF AN AIRPLANE.

INVESTIGATION OF MUTUAL INTERFERENCE EFFECTS OF SEVERAL VERTICAL-TALL-FUSELARGE CONFIGURATIONS IN SIDESLIP.

By Michael,William H. Naca, Washington 1954 . 22 , Bound With Naca Tn-3130-3134,3136-3139.

Place Hold on INVESTIGATION OF MUTUAL INTERFERENCE EFFECTS OF SEVERAL VERTICAL-TALL-FUSELARGE CONFIGURATIONS IN SIDESLIP.

CREEP BENDING AND BUCKLING OF LINEARLY VISCOELASTIC COLUMNS.

By Kempner,Joseph. Naca, Washington 1954 . 22 , Bound With Naca Tn-3130-3135,3137-3139.

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CREEP BENDING AND BUCKLING OF NONLINEARLY VISCOELASTIC COLUMNS.

By Kempner,Joseph. Naca, Washington 1954 . 27 , Bound With Naca Tn-3130-3136,3138-3139.

Place Hold on CREEP BENDING AND BUCKLING OF NONLINEARLY VISCOELASTIC COLUMNS.

CREEP BUCKLING OF COLUNS.

By Kempner,Joseph,Patel,Sharad A. Naca,Washington 1954 . 24 , Bound With Naca Tn-3130-3137,3139.

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TIME-DEPENDENT BUCKLING OF A UNIFORMLY HEATED COLUMN.

By Ness,Nathan. Naca,Washington 1954 . 18 , Bound With Naca Tn-3130-3138.

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A PROCEDURE FOR THE DESIGN OF AIR-HEATED ICE-PREVENTION SYSTEMS.

By Neel,Carr B. Naca, Washington 1954 . 63 , Bound With Naca Tn-3131-3139.

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EFFECT OF PRODUCT OF INERTIA ON LATERAL STABILITY.

By Sternfield,Leonard. Naca,Washington 1947 . 18 , Bound With Nasa Tn D-1190-1192,1194-1199.Lack Nos-1196,1197,1199

Place Hold on EFFECT OF PRODUCT OF INERTIA ON LATERAL STABILITY.

ROLLING AND YAWING MOMENTS FOR SWEPT-BACK WINGS IN SIDESLIP AT SUPERSONIC SPEEDS

By Lampert,Seymour. Naca, Washington . 55 , Bound With Naca Tn 2260-61,2263-70

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THE USE OF A LUMINESCENT LACQUER FOR THE VISUAL INDICATION OF BOUNDARY-LAYER TRANSITION

By Stalder,Jaction R. Naca, Washington . 17 , Bound With Naca Tn 2260-62,2264-70

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AIRFOIL PROFILES FOR MINIMUM PRESSURE DRAG AT SUPERSONIC VELOCITIES - GENERAL ANALYSIS WITH APPLICATION TO LINEARIZED SUPERSONIC FLOW

By Chapman,Dean R. Naca, Washington . 38 , Bound With Naca Tn 2260-63,2265-70

Place Hold on AIRFOIL PROFILES FOR MINIMUM PRESSURE DRAG AT SUPERSONIC VELOCITIES - GENERAL ANALYSIS WITH APPLICATION TO LINEARIZED SUPERSONIC FLOW

NACA VGH RECORDER

By Richardson,Norman R. Naca, Washington . 57 , Bound With Naca Tn 2260-64,2266-70

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INELASTIC COLUMN BEHAVIOR

By Duberg,John E. Naca, Washington . 44 , Bound With Naca Tn 2260-66,2268-70

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TESTS OF TWO-BLADE PROPELLERS IN THE LANGLEY 8-FOOT HIGH-SPEED TUNNEL TO DETERMINE THE EFFECT ON PROPELLER PERFORMANCE OF A MODIFICATION OF INBOARD PITCH DISTRIBUTION

By Delano,James B. Naca, Washington . 67 , Bound With Naca Tn 2260-67,2268-70

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A STRUCTURAL-EFFICIENCY EVALUATION OF TITANIUM AT NORMAL AND ELEVATED TEMPERATURES

By Heimerl,George J. Naca, Washington . 16 , Bound With Naca Tn 2260-68,2270

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THEORETICAL DAMPING IN ROLL AND ROLLING EFFECTIVENESS OF SLENDER CRUCIFORM WINGS

By Adams,Gaynor J. Naca, Washington . 30 , Bound With Naca Tn 2260-2269

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APPLICATION OF THE VON KARMAN MOMENTUM THEOREM TO TURBULENT BOUNDARY LAYERS

By Bidwell,Jerold M. Naca, Washington 1952 . 25 , Bound With Naca Tn 2570,2572-2579

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CERAMIC COATINGS FOR PREVENTION OF CARBON ABSORPTION IN FOUR HEAT-RESISTANT ALLOYS

By Pitts,J W. Naca, Washington 1972 . 14 , Bound With Naca Tn 2570-2571,2573-2579

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DEVELOPMENT OF AUXILIARY CYCLOTRON EQUIPMENT FOR TRIRIUM AS BOMBARDIND PATRICILES IN A CYCLOTRON

By Kundu,D N,Boyle,F G. Naca, Washington 1952 . 35 , Bound With Naca Tn 2570-2572,2574-2579

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A FLIGHT INVESTIGATION OF THE EFFECT OF CENTER-OF-GRAVITY LOCATION ON GUST LOADS

By Funk,Jack,Binckley,Earle T. Naca, Washington 1952 . 18 , Bound With Naca Tn 2770-2574,2576-2579

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A STUDY OF SLIP FORMATION IN POLYCRYSTALLINE ALUMINUM

By Johnson,Alide E,Batdorf,S B. Naca, Washington 1952 . 18 , Bound With Naca Tn 2570-2575,2577-2579

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ON THE ANGULAR DISTRIBUTION OF SLIP LINES IN POLYCRYSTALLINE ALIMINUM ALLOY

By Hedgepeth,J M,Batdorf,S B. Naca, Washington 1952 . 18 , Bound With Naca 2570-2576,2578-2579

Place Hold on ON THE ANGULAR DISTRIBUTION OF SLIP LINES IN POLYCRYSTALLINE ALIMINUM ALLOY

A COMPARISON OF PREDICATED AND EXPERIMENTALLY DETERMINED LONGITTUINAL DYNAMIC RESPONSES OF A STABILIZED AIRPLANE

By Smaus,Louis H,Gore,Marvin R. Naca, Washington 1952 . 53 , Bound With Naca Tn 2570-2577,2579

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APPROXIMATE METHODS FOR CALCULATING THE FLOW ABOUT NONLIFTING BODIES OF REVOLUTION AT HIGH SUPERSONIC AIRSPEEDS

By Eggers,A J. Naca, Washington 1952 . 40 , Bound Wit Naca Tn 2570-2578

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SAFEGUARDS AGAINST FLUTTER OF AIRPLANES

By Vries,Gerhard De. Naca, Washington 1956 . 94 , Bound With Naca 1420-22,1424-29

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ON THE THEORY OF ANISOTROPIC SHALLOW SHELLS

By Ambartsumyan,S A. Naca, Washington 1956 . 11 , Bound With Naca 1420-23,1425-29

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ON THE CALCULATION OF SHALLOW SHELLS

By Ambartsumyan,S A. Naca, Washington 1956 . 11 , Bound With Naca 1420-24,1426-29

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ON THE THEORY OF THIN SHALLOW SHELLS

By Nazarov,A A. Naca, Washington 1956 . 7 , Bound With Naca 1420-25,1427-29

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TURBULENCE IN THE WAKE OF A THIN AIRFOIL AT LOW SPEEDS

By Campbell,George S. Naca, Washington 1957 . 63 , Bound With Naca 1420-1426,1428-29

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EFFECT OF FATIGUE CRACK ON STATIC STRENGTH

By Nordmark,Glenn E. Naca, Washington 1957 . 22 , Bound With Naca 1420-27, 1429

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WALL LNTERFERENCE IN A PERFORATED WIND TUNNEL

By Brescia,Riccardo. Naca, Washington 1957 . 28 , Bound With Naca 1420-28

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COMPARISON OF AIRSPEED CALIBRATIONS EVELUATED BY THE ACCELEROMETER AND RADAR METHODS

By Lina,Lindsay J,Trant,James P. Naca,Washington 1952 . 16 , Bound With Naca Tn 2571-2579

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INCOMPRESSIBLE FLUTTER CHARACTERISTICS OF REPRESENTATIVE AIRCRAFT WINGS

By Wilts,C H. Naca, Washington 1957 . 121 , Bound With Naca Tn 3781-89.

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WORKING CHARTS FOR THE DETERMINATION OF PROPELLER THRUST AT VARIOUS AIR SPEEDS.

By Hartman,Edwin P. Naca, Washington 1934 . 21 , Bound With Naca-482-500.

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MEASUREMENTS OF THE EFFECT OF TRAILING-EDGE THICKNESS ON THE ZERO-LIFT DRAG OF THIN LOW -ASPECT-RATIO WINGS

By Morrow,John D. Naca, Washington 1955 . 11 , Bound With Naca Tn 3551-3559

Place Hold on MEASUREMENTS OF THE EFFECT OF TRAILING-EDGE THICKNESS ON THE ZERO-LIFT DRAG OF THIN LOW -ASPECT-RATIO WINGS

SYNTHESIS AND PURIFICATION OF SOME ALKYLBIPHENYLS AND ALKYLBCYCLOHEXYLS

By Goodman,Irving A,Wise,Paul H. Naca, Washington 1951 . 29 , Bound With Naca Tn 2261-70

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NOTE ON REASEARCH WORK BY HELMHOLZ AND WIEN RELATING TO THE WAVES PROPGATED ALONG THE SURFACE OF SEPRATION OF TWO LIQUIDS

By BURBERGERS,J M. NACA,WASHINGTON 1928 . ,8,,,,,, , Bound with NACA TM-470,465.

Place Hold on NOTE ON REASEARCH WORK BY HELMHOLZ AND WIEN RELATING TO THE WAVES PROPGATED ALONG THE SURFACE OF SEPRATION OF TWO LIQUIDS

A Digital automatic multiple pressure recorder

By Coss, Bert A.. Washington, D. C. NACA 1953 . 24p

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Aerodynamic characteristics of a two-blade NACA 10-(3)(062)-045 propeller and of a two-blade NACA 10-(3)(08)-045 propeller

By Solomon, William. Washington, D. C. NACA 1953 . 53p

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Bearing Strengths of Some 75S-T6 and 14S-T6 Aluminum-alloy Hand Forgings

By Finley, E. M.. Wasington, D. C. NACA 1953 . 40p

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An analysis of statically indeterminate trusses having members stressed beyond the proportional limit

By Wilder, Thomas W . Washington, D. C. NACA 1953 . 13p

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Some exact solutions of two-dimensional flows of compressible fluid with hodograph method

By Chien-Chien, Chang. Washington, D. C. NACA 1953 . 63p

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An analysis of statically indeterminate trusses having members stressed beyond the proportional limit

By Wilder, Thomas W. . Washington, D. C. NACA 1953 . 13p

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On the stability of the laminar mixing region between two parallel streams in a gas

By Lin, C. C. . Washington, D. C. NACA 1953 . 50p

Place Hold on On the stability of the laminar mixing region between two parallel streams in a gas

Performance Characteristics of Plane-Wall Two-Dimensional Diffusers [NACA-TN-2888]

By Elliott, G Reid. National Advisory Committee for Aeronautics NACA 1953 . 80p

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Estimation of Hydrodynamic Impact Loads and Pressure Distributions on Bodies Approximating Elliptical Cylinders with Special Reference to Water Landings of Helicopters [NACA TN-2889]

By Schnitzer, Emanuel. Washington, D. C. NACA 1953 . 31p

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Shearing-stress Measurements by use of A Heated Element

By Liepmann .H.W. Washington National Advisory Committee for Aeronautics [NACA TN-3268] 1954 . 27

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Effect of Dissociation on Thermodynamic Properties of Pure Diatomic Gases (TN 3270)

By Woolley , Harold . W. Washington National Advisory Committee for Aeronautics [NACA TN-3270] 1955 . 19

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National advisory committee for aeronautics [NASA TN D-4320 -- TN D-4329]

By Ostrach, Simon. Washington NACA 1958 . 18p , Bound with Nasa TN D-4320 to TN D- 4329 [Accession Nos: 68218 to 68218(i)

Place Hold on National advisory committee for aeronautics [NASA TN D-4320 -- TN D-4329]

An application of lifting -surface theory to the prediction of angle-of -attack hinge - moment parameters for aspect ratio 4.5 wings [NASA TN D-1420 -- TN D-1429]

By Jones, L.. Washington NACA 1947 . 16p , Bound with NACA TN-1420 to TN-1429 Lacks Nos 1422,1426,1428

Place Hold on An application of lifting -surface theory to the prediction of angle-of -attack hinge - moment parameters for aspect ratio 4.5 wings [NASA TN D-1420 -- TN D-1429]