PKK Library Search for 'se,phr:"National Advisory Committee for Aeronautics"'

COMPARISON OF SEVERAL METHODS FOR OBTAINING THE TIME RESPONSE OF LINEAR SYSTEMS TO EITHER A UNIT IMPULSE OR ARBITRARY INPUT FROM FREQUENCY-RESPONSE DATA

By Donegan,James J.. 1957

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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

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

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

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

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

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

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

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

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

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

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

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

LOW-SPEED DRAG OF CYLINDERS OF VARIOUS SHAPES

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

Place Hold on LOW-SPEED DRAG OF CYLINDERS OF VARIOUS SHAPES

EXPERIMENTAL STRESS ANALYSIS OF STIFFENED CYLINDERS WITH COTOUTS

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

Place Hold on EXPERIMENTAL STRESS ANALYSIS OF STIFFENED CYLINDERS WITH COTOUTS

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

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

A Digital automatic multiple pressure recorder

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

Place Hold on A Digital automatic multiple pressure recorder

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

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

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

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

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

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

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

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

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

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

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

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

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

Smoke of nozzle secondary flows in a low speed turbine [TN 3260]

By Kofskey, Milton G.. Washington National Advisory Committee for Aeronautics 1954 . 24p

Place Hold on Smoke of nozzle secondary flows in a low speed turbine [TN 3260]

Airfoil section characterstics as applied to the prediction of air forces and their distribution on wings[R.No.631]

By Jacobs,Eastman N.. Washington,D.C. National Advisory Committee For Aeronautics 1938 . 29p.

Place Hold on Airfoil section characterstics as applied to the prediction of air forces and their distribution on wings[R.No.631]

The crinkling strength and the bending strength of round aircraft tubing[R.No632].

Washington,D.C. National Advisory Committee For Aeronautics 1938 . 15p.

Place Hold on The crinkling strength and the bending strength of round aircraft tubing[R.No632].

Pressure distribution over an N.A.C.A.23012 airfoil with a slotted and a plan flap

By Wenzinger,Carl J.. Washington,D.C. National Advisory Committee For Aeronautics 1938 . 32p.

Place Hold on Pressure distribution over an N.A.C.A.23012 airfoil with a slotted and a plan flap

Calculation of the chordwise load distribution over airfoil sections with plain,split,or serially hinged traniling-edge flaps[R.No.634]

By Allen,H.Julian. Washington,D.C. National Advisory Committee For Aeronautics 1938 . 16p.

Place Hold on Calculation of the chordwise load distribution over airfoil sections with plain,split,or serially hinged traniling-edge flaps[R.No.634]

Theoretical stability and control characteristics of wings with various amounts of taper and twist [R.No.635]

By Pearson,Henry A.. Washington,D.C National Advisory Committee For Aeronautics 1938 . 17p

Place Hold on Theoretical stability and control characteristics of wings with various amounts of taper and twist [R.No.635]

Approximate stress analysis of multi-stringer beams with shear deformation of the flanges[R.No.636]

By Kuhn,Paul. Washington,D.C. National advisory committee for aeronautics 1938 . 21p.

Place Hold on Approximate stress analysis of multi-stringer beams with shear deformation of the flanges[R.No.636]

Determination of boundary layer transition on three symmetrical airfoils in the N.A.C.A. full scale wind tunnel [R. No.637]

By Silverstein, Abe. Washington,D.C. National Advisory Committee for Aeronautics 1939 . 15p

Place Hold on Determination of boundary layer transition on three symmetrical airfoils in the N.A.C.A. full scale wind tunnel [R. No.637]

The infulence of lateral stability on disturbed motions of an airplane with special reference to the motions produced by gusts [R.No. 638]

By Jones, Robert T.. Washington, D.C. National Advisory Committee for Aeronautics 1938 . 10p

Place Hold on The infulence of lateral stability on disturbed motions of an airplane with special reference to the motions produced by gusts [R.No. 638]

The effect of compressibility on eight full-scale propellers operating in the take-off and climbing range[R.No.639]

By Biermann,David. Washington,D.C. National Advisory Committee For Aeronautics 1938 . 29p.

Place Hold on The effect of compressibility on eight full-scale propellers operating in the take-off and climbing range[R.No.639]

The aerodynamic characteristics of full-scale propellers having 2,3, and 4 blabes of clark Y and R.A.F.6 airfoil sections[R.No.640]

By Hartman,Edwin P.. Washington.D.C. National Advisory Committee For Aeronautics 1938 . 23p.

Place Hold on The aerodynamic characteristics of full-scale propellers having 2,3, and 4 blabes of clark Y and R.A.F.6 airfoil sections[R.No.640]

Measurement and power spectra of runway roughness at airports in countries of the north atlantic treaty organization [Technical Note-4303]

By Thompson,Wilbur E.. Washington National Advisory Committee for Aeronautics 1958 . 85p

Place Hold on Measurement and power spectra of runway roughness at airports in countries of the north atlantic treaty organization [Technical Note-4303]

Matrix method for obraining spanwise moments and deflections of torsionally rigis rotor blades with arbitrary loadings [Technical Note 4304]

By Mayo, Alton P.. Washington National Advisory Committee for Aeronautics 1958 . 51p

Place Hold on Matrix method for obraining spanwise moments and deflections of torsionally rigis rotor blades with arbitrary loadings [Technical Note 4304]

Wind tunnel investigation of effects ofspoilerocation, spoiler size, and fuselage nose shape on directional charecteristics of a model of a model of a tandem-rotor helicopter fuselage [NACA TN-4305]

By Williams, James L.. Washington National Advisory Committee for Aeronautics 1958 . 44p

Place Hold on Wind tunnel investigation of effects ofspoilerocation, spoiler size, and fuselage nose shape on directional charecteristics of a model of a model of a tandem-rotor helicopter fuselage [NACA TN-4305]

Temperature and thermal stress distributions in some structural elements heated at a constant rate [NACA TN-4306]

By Brooks, William A.. Washington National Advisory Committe for Aeronautics 1958 . 77p

Place Hold on Temperature and thermal stress distributions in some structural elements heated at a constant rate [NACA TN-4306]

Transient temperature distribution in two component semi infinite composite slab of arbitrary materials subjected to aerodynamic heating with a discontinuous change in equilibrium temperature or heat transfer coefficient [Technical Note 4308]

By Trimpi, Robert L.. Washington National Advisory Committee for Aeronautics 1958 . 83p

Place Hold on Transient temperature distribution in two component semi infinite composite slab of arbitrary materials subjected to aerodynamic heating with a discontinuous change in equilibrium temperature or heat transfer coefficient [Technical Note 4308]

Experimental measurements of the effects of airplane motions on wing and tail angles of attack of a swept wing bomber in rough air [NACA TN-4307]

By Engel, Jerome N.. Washington, D. C. National Advisory Committee for Aeronautics 1958

Place Hold on Experimental measurements of the effects of airplane motions on wing and tail angles of attack of a swept wing bomber in rough air [NACA TN-4307]

Use of shotr flat vanes for producing efficient wide angle two-dimensional subsonic diffusers [NACA TN-4309]

By Cochran, D. L.. Washington National Advisory Committee for Aeronautics 1958 . 135p

Place Hold on Use of shotr flat vanes for producing efficient wide angle two-dimensional subsonic diffusers [NACA TN-4309]

A method for evaluating the effects of drag and inlet presuure recovery on propulsion system performance [NACA Note-3261]

By Kremzier, Emil J.. Washington , D. C. National Advisory Committee for Aeronautics 1954 . 21p

Place Hold on A method for evaluating the effects of drag and inlet presuure recovery on propulsion system performance [NACA Note-3261]

A method for evaluating the effects of drag and inlet pressure recovery on propulsion system performance [ Technical Note 3261 ]

By Kremzier, Email J.. Washington National Advisory committee for Aeronautics 1954 . 21p

Place Hold on A method for evaluating the effects of drag and inlet pressure recovery on propulsion system performance [ Technical Note 3261 ]

Starting and operating limits of two supersonic wind tunnels utilizing auxiliary air injection downstream of the test section [ Technical Note 3262 ]

By Hunczak, Henry R.. Washington National Advisory Committee for Aeronautics 1954 . 26p

Place Hold on Starting and operating limits of two supersonic wind tunnels utilizing auxiliary air injection downstream of the test section [ Technical Note 3262 ]

Lift and moment equations for oscillating airfouls in an infinite unstaggered cascade [TN-3263]

By Mendelson, Alexander. Washington National Advisory Committee for Aeronautics 1954 . 46p

Place Hold on Lift and moment equations for oscillating airfouls in an infinite unstaggered cascade [TN-3263]

Study of the momentum distribution of turbulent boundary layers in adverse pressure gradients [Technical Note 3264]

By Sandborn, Virgil A.. Washington National Advisory Committee for Aeronautics 1955 . 79p

Place Hold on Study of the momentum distribution of turbulent boundary layers in adverse pressure gradients [Technical Note 3264]

Study of the momentum distribution of turbulent boundary layers in adverse pressure gradients [Technical Note 3264]

By Sandborn, Virgil A.. Washington National Advisory Committee for Aeronautics 1955 . 79p

Place Hold on Study of the momentum distribution of turbulent boundary layers in adverse pressure gradients [Technical Note 3264]

Vaporization rates and drag coefficients for isooctane sprays in turbulent air streams [TN-3265]

By Ingebo, Robert D.. Washington National Advisory Committee for Aeronautics 1954 . 39p

Place Hold on Vaporization rates and drag coefficients for isooctane sprays in turbulent air streams [TN-3265]

Experimental evaluation of momentum terms in turbulent pipe flow [Technical Note 3266]

By Sandborn, Virgil A.. Washington National Advisory Committee for Aeronautics 1955 . 40p

Place Hold on Experimental evaluation of momentum terms in turbulent pipe flow [Technical Note 3266]

Boundary layer transition at mach 3.12 with and wihtout single roughness elements [Technical Note 3267]

By Brinich, Paul F.. Washington National Advisory Committee for Aeronautics 1954 . 41p

Place Hold on Boundary layer transition at mach 3.12 with and wihtout single roughness elements [Technical Note 3267]

Compressible flow about symmetrical joukowski profiles [Report No. 621]

By Kaplan, Carl. Washington,D.C. National Advisory Committee for Aeronautics 1938 . 15p

Place Hold on Compressible flow about symmetrical joukowski profiles [Report No. 621]

A photographic study of combustion and knock in a spark ignition engine [Report No.622]

By Rothrock,A.M.. Washington,D.C. National Advisory Committee for Aeronautics 1938 . 21p

Place Hold on A photographic study of combustion and knock in a spark ignition engine [Report No.622]

A study of the torque equilibrium of an autogiro rotor [Report No.623]

By Bailey,F.J.. Washington,D.C. National Advisory Committee for Aeronautics 1938 . 10p

Place Hold on A study of the torque equilibrium of an autogiro rotor [Report No.623]

Two Dimensional subsonic compressible flow past elliptic cylinders [Report No.624]

By Kaplan, Carl. Washington,D.C. National Advisory Committee for Aeronautics 1938 . 8p

Place Hold on Two Dimensional subsonic compressible flow past elliptic cylinders [Report No.624]

The Tranistion phase inthe take off of an airplane [Report No.626]

By Wetmore,J.W.. Washington,D.C. National Advisory Committee for Aeronautics 1938 . 11p

Place Hold on The Tranistion phase inthe take off of an airplane [Report No.626]

The experimental and calculated characteristics of 22 tapered wings [Report No.627]

By Anderson,Raymond F.. Washington,D.C. National Advisory committee for Aeronautics 1938 . 23p

Place Hold on The experimental and calculated characteristics of 22 tapered wings [Report No.627]

Aerodynamic characteristics of a large number of airpoils tested in the variable density wind tunnel [Report No.628]

By Pinkerton,Robert M.. Washington,D.C. National Advisory committee for Aeronautics 1938 . 49p

Place Hold on Aerodynamic characteristics of a large number of airpoils tested in the variable density wind tunnel [Report No.628]

On some reciprocal relations in the theory of nonstationary flows [Report No.629]

By Garrick, I.E.. Washington,D.C. National Advisory committee for Aeronautics 1938 . 4p

Place Hold on On some reciprocal relations in the theory of nonstationary flows [Report No.629]

A flight comparison of conventional ailerons on a rectangular wing and of conventional and floating wing tip ailerons on a tapered wing [Report No.630]

By Soule,H.A.. Washington,D.C. National Advisory Committee for Aeronautics 1938 . 5p

Place Hold on A flight comparison of conventional ailerons on a rectangular wing and of conventional and floating wing tip ailerons on a tapered wing [Report No.630]

The drag of two streamline bodies as affected by protuberances and appendages [Report No. 451]

By Abbott, Ira H.. Washington, D. C. National Advisory Committee for Aeronautics 1932 . 8p

Place Hold on The drag of two streamline bodies as affected by protuberances and appendages [Report No. 451]

General potential theory of arbitrary wing sections [Report no. 452]

By Theodorsen, T.. Washington, D. C. National Advisory Committee for Aeronautics 1940 . 35p

Place Hold on General potential theory of arbitrary wing sections [Report no. 452]

The estimation of maximum load capacity of seaplanes and flying boats[Report no. 453]

By Diehl, Walter S.. Washington, D. C. National Advisory Committee for Aeronautics 1932 . 27p

Place Hold on The estimation of maximum load capacity of seaplanes and flying boats[Report no. 453]

The estimation of maximum load capacity of seaplanes and flying boats[Report no. 453]

By Diehl, Walter S.. Washington, D. C. National Advisory Committee for Aeronautics 1932 . 27p

Place Hold on The estimation of maximum load capacity of seaplanes and flying boats[Report no. 453]

Penetration and duration of fuel sprays from a pump injection system [Report no. 455]

By Rothrock, A. M.. Washington, D. C. National Advisory Committee for Aeronautics 1933 . 10p

Place Hold on Penetration and duration of fuel sprays from a pump injection system [Report no. 455]

The aerodynamic forces and moments exerted on a spinning model of the NY-1 airplane as measured by the spinning balance [Report no. 456]

By Bamber, M. J.. Washington, D. C. National Advisory Committee for Aeronautics 1933 . 15p

Place Hold on The aerodynamic forces and moments exerted on a spinning model of the NY-1 airplane as measured by the spinning balance [Report no. 456]

Maneuverability investigation of an o3u observation airplane [Report no. 457]

By Thompson, F. L.. Washington, D. C. National Advisory Committee for Aeronautics 1933 . 14p

Place Hold on Maneuverability investigation of an o3u observation airplane [Report no. 457]

Relative loading on biplane wings [Report no. 458]

By Diehl, Walter S.. Washington, D. C. National Advisory Committee for Aeronautics 1933 . 17p

Place Hold on Relative loading on biplane wings [Report no. 458]

The N. A. C. A. full scale wind tunnel [Report no. 459]

By France, Smith J. De. Washington, D. C. National Advisory Committee for Aeronautics 1933 . 10p

Place Hold on The N. A. C. A. full scale wind tunnel [Report no. 459]

The charectristics of 78 related airfoil sections from tests in the variable density wind tunnel [Report no. 460]

By Jacobs, Eastman N.. Washington, D. C. National Advisory Committee for Aeronautics 1933 . 58p

Place Hold on The charectristics of 78 related airfoil sections from tests in the variable density wind tunnel [Report no. 460]