PKK Library Search for 'su:{Aerodynamics} and se:National Aeronautics and Space Administration'

TRANSONIC FLOW FIELD ANALYSIS FOR WING-FUSELAGE CONFIGURATIONS

By Boppe, Charles W.. Washington National Aeronautics And Space And Administration 1980 . vii,152

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NASA Technical Note [NASA TN D-5016]: Aerodynamic data on large semispan tilting wing with 0.4-diameter chord, single-slotted flap and single propeller 0.22 chord below wing

Washington NASA 1969 . 203p , Bound together NASA TN D-5011 to 5020 | Bound vol. Acc. No. 101131 contains Acc. No. TR8236 to TR8244

Place Hold on NASA Technical Note [NASA TN D-5016]: Aerodynamic data on large semispan tilting wing with 0.4-diameter chord, single-slotted flap and single propeller 0.22 chord below wing

NASA Technical Note [NASA TN D-3442]: Low-subsonic wind-tunnel and free-flight drop-test investigation of a paraglider configuration having large tapered leading edges and keel

Washington NASA 1966 . 32p , Bound together NASA TN D-3441 to 3450 | Bound vol. Acc. No. 64324 contains Acc. No. TR8886 to TR8894

Place Hold on NASA Technical Note [NASA TN D-3442]: Low-subsonic wind-tunnel and free-flight drop-test investigation of a paraglider configuration having large tapered leading edges and keel

NASA Technical Note [NASA TN D-2546]: Use of arbitrary quasi-orthogonals for calculating flow distribution in the meridional plane of a turbomachine

Washington NASA 1964 . 46p , Bound together NASA TN D-2541 to 2550 | Bound vol. Acc. No. 67642 contains Acc. No. TR9902 to TR9910

Place Hold on NASA Technical Note [NASA TN D-2546]: Use of arbitrary quasi-orthogonals for calculating flow distribution in the meridional plane of a turbomachine

NASA Technical Note [NASA TN D-3122]: Performance characteristics of a 4-foot-diameter ducted fan at zero angle of attack for several fan blade angles

Washington NASA 1965 . 17p , Bound together NASA TN D-3121 to 3130 | Bound vol. Acc. No. 63217 contains Acc. No. TR8723 to TR8731

Place Hold on NASA Technical Note [NASA TN D-3122]: Performance characteristics of a 4-foot-diameter ducted fan at zero angle of attack for several fan blade angles

NASA Technical Note [NASA TN D-3126]: Strain measurements conducted on a full scale echo ii passive communications satellite balloon

Washington NASA 1966 . 23p , Bound together NASA TN D-3121 to 3130 | Bound vol. Acc. No. 63217 contains Acc. No. TR8723 to TR8731

Place Hold on NASA Technical Note [NASA TN D-3126]: Strain measurements conducted on a full scale echo ii passive communications satellite balloon

NASA Technical Note [NASA TN D-5932]: Full-scale wind-tunnel investigation of the aerodynamic characteristics of the x-24a lifting body aircraft

Washington NASA 1970 . 54p , Bound together NASA TN D-5930 to 5939 | Bound vol. Acc. No. 101211 contains Acc. No. TR7877 to TR7885

Place Hold on NASA Technical Note [NASA TN D-5932]: Full-scale wind-tunnel investigation of the aerodynamic characteristics of the x-24a lifting body aircraft

NASA Technical Note [NASA TN D-4329]: Measurements of ground effect on a low-aspect-ratio ogee-wing airplane model and calculations of landing-flare trajectories

Washington NASA 1968 . 38p , Bound together NASA TN D-4321 to 4330 | Bound vol. Acc. No. 86052 contains Acc. No. TR8602 to TR8610

Place Hold on NASA Technical Note [NASA TN D-4329]: Measurements of ground effect on a low-aspect-ratio ogee-wing airplane model and calculations of landing-flare trajectories

NASA Technical Note [NASA TN D-2547]: Energy transfer from a liquid to gas bubbles forming at a submerged orifice

Washington NASA 1965 . 178p , Bound together NASA TN D-2541 to 2550 | Bound vol. Acc. No. 67642 contains Acc. No. TR9902 to TR9910

Place Hold on NASA Technical Note [NASA TN D-2547]: Energy transfer from a liquid to gas bubbles forming at a submerged orifice

NASA Technical Note [NASA TN D-2550]: Application of generalized Newtonian theory to three-dimensional sharp-nose shock-detached bodies at mach for angles of attack up to 25 [degree]

Washington NASA 1965 . 41p , Bound together NASA TN D-2541 to 2550 | Bound vol. Acc. No. 67642 contains Acc. No. TR9902 to TR9910

Place Hold on NASA Technical Note [NASA TN D-2550]: Application of generalized Newtonian theory to three-dimensional sharp-nose shock-detached bodies at mach for angles of attack up to 25 [degree]

NASA Technical Note [NASA TN D-446]: Some examples of the applications of the transonic and supersonic area rules to the prediction of wave drag

Washington NASA 1960 . 46p , Bound together NASA TN D-441 to 450 | Bound vol. Acc. No. 63667 contains Acc. No. TR10185 to TR10193

Place Hold on NASA Technical Note [NASA TN D-446]: Some examples of the applications of the transonic and supersonic area rules to the prediction of wave drag

NASA Contractor Report [NASA CR-2309]: Simulator tests to study hot-flow problems related to a gas core reactor

Washington NASA 1973 . iv,112p , Bound together NASA CR-2308 to 2314 Lack No. 2313 | Bound vol. Acc. No. 101610 contains Acc. No. TR8548 to TR8550 | NASA CR-2314 [This report no. doesn't have Acc. No.] -- The distribution of odd nitrogen in the lower stratosphere and possible perturbations caused by stratospheric air transport/ Ivar S. A. Isaksen and Eigil Hesstvedt

Place Hold on NASA Contractor Report [NASA CR-2309]: Simulator tests to study hot-flow problems related to a gas core reactor

NASA Technical Note [NASA TN D-2853]: Aerodynamic characteristics of a family of multistage missiles at a mach number of 6.0

Washington NASA 1965 . 29p , Bound together NASA TN D-2851 to 2860 | Bound vol. Acc. No. 64286 contains Acc. No. TR10215 to TR10223

Place Hold on NASA Technical Note [NASA TN D-2853]: Aerodynamic characteristics of a family of multistage missiles at a mach number of 6.0

NASA Technical Note [NASA TN D-2854]: A parametric study of the aerodynamic characteristics of nose-cylinder-flare bodies at a mach number of 6.0

Washington NASA 1965 . 74p , Bound together NASA TN D-2851 to 2860 | Bound vol. Acc. No. 64286 contains Acc. No. TR10215 to TR10223

Place Hold on NASA Technical Note [NASA TN D-2854]: A parametric study of the aerodynamic characteristics of nose-cylinder-flare bodies at a mach number of 6.0

NASA Technical Note [NASA TN D-2855]: Relationship between the aerodynamic damping derivatives measured as a function of instantaneous angular displacement and the aerodynamic damping derivatives measured as a function of oscillation amplitude

Washington NASA 1965 . 16p , Bound together NASA TN D-2851 to 2860 | Bound vol. Acc. No. 64286 contains Acc. No. TR10215 to TR10223

Place Hold on NASA Technical Note [NASA TN D-2855]: Relationship between the aerodynamic damping derivatives measured as a function of instantaneous angular displacement and the aerodynamic damping derivatives measured as a function of oscillation amplitude

NASA Technical Note [NASA TN D-2859]: Low-speed wind tunnel tests of a large-scale inflatable structure paraglider

Washington NASA 1965 . 30p , Bound together NASA TN D-2851 to 2860 | Bound vol. Acc. No. 64286 contains Acc. No. TR10215 to TR10223

Place Hold on NASA Technical Note [NASA TN D-2859]: Low-speed wind tunnel tests of a large-scale inflatable structure paraglider

NASA Technical Note [NASA TN D-1942]: Application of dorodnitsyn's integral method to nonequilibrium flows over pointed bodies

Washington NASA 1963 . 43p , Bound together NASA TN D-1941 to 1950 | Bound vol. Acc. No. 65584 contains Acc. No. TR10692 to TR10700

Place Hold on NASA Technical Note [NASA TN D-1942]: Application of dorodnitsyn's integral method to nonequilibrium flows over pointed bodies

NASA Technical Note [NASA TN D-1949]: Flutter of flat rectangular orthotropic panels with biaxial loading and arbitrary flow direction

Washington NASA 1963 . 33p , Bound together NASA TN D-1941 to 1950 | Bound vol. Acc. No. 65584 contains Acc. No. TR10692 to TR10700

Place Hold on NASA Technical Note [NASA TN D-1949]: Flutter of flat rectangular orthotropic panels with biaxial loading and arbitrary flow direction

NASA Technical Note [NASA TN D-3022]: Evaluation of the lateral-directional stability and control characteristics of the lightweight M2-F1 lifting body at low speed

Washington NASA 1965 . 34p , Bound together NASA TN D-3021 to 3030 | Bound vol. Acc. No. 64302 contains Acc. No. TR10442 to TR10450

Place Hold on NASA Technical Note [NASA TN D-3022]: Evaluation of the lateral-directional stability and control characteristics of the lightweight M2-F1 lifting body at low speed

NASA Technical Note [NASA TN D-3025]: Effect of wing planform modification on longitudinal characteristics of a variable-sweep M wing

Washington NASA 1965 . 26p , Bound together NASA TN D-3021 to 3030

Place Hold on NASA Technical Note [NASA TN D-3025]: Effect of wing planform modification on longitudinal characteristics of a variable-sweep M wing

NASA Technical Note [NASA TN D-3027]: Illustration of design methods for power reduction in logical systems

Washington NASA 1965 . 19p , Bound together NASA TN D-3021 to 3030 | Bound vol. Acc. No. 64302 contains Acc. No. TR10442 to TR10450

Place Hold on NASA Technical Note [NASA TN D-3027]: Illustration of design methods for power reduction in logical systems

NASA Technical Note [NASA TN D-6292]: Experimental investigation of the use of slotted test-section walls to reduce wall interference for high-lift-model testing

Washington NASA 1971 . 72p , Bound together NASA TN D-6290 to 6299 | Bound vol. Acc. No. 101242 contains Acc. No. TR11521 to TR11529

Place Hold on NASA Technical Note [NASA TN D-6292]: Experimental investigation of the use of slotted test-section walls to reduce wall interference for high-lift-model testing

NASA Technical Note [NASA TN D-6117]: Utilization of a fixed-base simulator to study the stall and spin characteristics of fighter airplanes

Washington NASA 1971 . 34p , Bound together NASA TN D-6110 to 6118 | Bound vol. Acc. No. 101227 contains Acc. No. TR13899 to TR13906

Place Hold on NASA Technical Note [NASA TN D-6117]: Utilization of a fixed-base simulator to study the stall and spin characteristics of fighter airplanes

NASA Technical Note [NASA TN D-5661]: Design charts of static and rotary stability derivatives for cropped double-delta wings in subsonic compressible flow

Washington NASA 1970 . 79p , Bound together NASA TN D-5660 to 5669 | Bound vol. Acc. No. 101185 contains Acc. No. TR14371 to TR14379

Place Hold on NASA Technical Note [NASA TN D-5661]: Design charts of static and rotary stability derivatives for cropped double-delta wings in subsonic compressible flow

NASA Technical Note [NASA TN D-5662]: Effects of ground proximity on the longitudinal aerodynamic characteristics of an unswept aspect-ratio-10 wing

Washington NASA 1970 . 60p , Bound together NASA TN D-5660 to 5669 | Bound vol. Acc. No. 101185 contains Acc. No. TR14371 to TR14379

Place Hold on NASA Technical Note [NASA TN D-5662]: Effects of ground proximity on the longitudinal aerodynamic characteristics of an unswept aspect-ratio-10 wing

NASA TN [D-6553]

By Fishbach, Lanrence H.. NASA, Washington, D.C. 1972 . 184p , NASA Technical Note D-6552,53,57,63,68 Bounded Volumes Accession No. 101251; Contents: TR13142-46

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NASA TN [D-6556]

By Anderson, Douglas A.. NASA, Washington, D.C. 1971 . 51p , NASA Technical Note D-6552,53,57,63,68 Bounded Volumes Accession No. 101251; Contents: TR13142-46

Place Hold on NASA TN [D-6556]

NASA Technical Note [NASA TN D-545]: A note on the drag due to lift of delta wings at mach numbers up to 2.0

Washington NASA 1960 . 14p , Bound together NASA TN D-541 to 550 | Bound vol. Acc. No. 65466 contains Acc. No. TR15854 to TR15862

Place Hold on NASA Technical Note [NASA TN D-545]: A note on the drag due to lift of delta wings at mach numbers up to 2.0

NASA Technical Note [NASA TN D-549]: Heat-transfer measurements at a mach number of 4.95 on two 60 [degree] swept delta wings with blunt leading edges and dihedral angles of 0 [degree] and 45 [degree]

Washington NASA 1961 . 50p , Bound together NASA TN D-541 to 550 | Bound vol. Acc. No. 65466 contains Acc. No. TR15854 to TR15862

Place Hold on NASA Technical Note [NASA TN D-549]: Heat-transfer measurements at a mach number of 4.95 on two 60 [degree] swept delta wings with blunt leading edges and dihedral angles of 0 [degree] and 45 [degree]

Effects of configutation modifications on aerodynamic charectristics of tension shell shapes at mach 3.0 [NASA TN D-4080]

By Sawyer, James Wayne. Washington, D. C. National Aeronautics and Space Administration . 37p

Place Hold on Effects of configutation modifications on aerodynamic charectristics of tension shell shapes at mach 3.0 [NASA TN D-4080]

NASA Technical Note [NASA TN D-383]: Theoretical calculations of the pressures forces, and moments due to various lateral motions acting on tapered sweptback vertical tails with supersonic leading and trailing edges

Washington NASA 1960 . 126p , Bound together NASA TN D-381 to 390 | Bound vol. Acc. No. 63662 contains Acc. No. TR15585 to TR15589, TR15610, TR15590 to TR15591 & TR15611

Place Hold on NASA Technical Note [NASA TN D-383]: Theoretical calculations of the pressures forces, and moments due to various lateral motions acting on tapered sweptback vertical tails with supersonic leading and trailing edges

NASA Technical Note [NASA TN D-389]: The longitudinal aerodynamic characteristics of a sweptback wing-body combination with and without end plates at mach numbers from 0.40 to 0.93

Washington NASA 1960 . 22p , Bound together NASA TN D-381 to 390 | Bound vol. Acc. No. 63662 contains Acc. No. TR15585 to TR15589, TR15610, TR15590 to TR15591 & TR15611

Place Hold on NASA Technical Note [NASA TN D-389]: The longitudinal aerodynamic characteristics of a sweptback wing-body combination with and without end plates at mach numbers from 0.40 to 0.93

NASA Technical Note [NASA TN D-390]: Aerodynamic characteristics of a 1/4-scale model of a tilt-wing VTOL aircraft at high angles of wing incidence

Washington NASA 1960 . 42p , Bound together NASA TN D-381 to 390 | Bound vol. Acc. No. 63662 contains Acc. No. TR15585 to TR15589, TR15610, TR15590 to TR15591 & TR15611

Place Hold on NASA Technical Note [NASA TN D-390]: Aerodynamic characteristics of a 1/4-scale model of a tilt-wing VTOL aircraft at high angles of wing incidence

MARKED INFLUENCE OF CRYSTAL STRUCTURE ON THE FRICTION AND WEAR CHARACTERISTICS OF COBALT AND COBALT BASE ALLOYS IN VACUUM TO 10-9 MILLIMETER OF MERCURY II-COBALT ALLOYS

By Buckley,Donlad H.. NASA, Washington, D.C. 1964 . 8 , Technical Reports D-2521-30 Bound Vol. No.83082; Contents: TR16210-218

Place Hold on MARKED INFLUENCE OF CRYSTAL STRUCTURE ON THE FRICTION AND WEAR CHARACTERISTICS OF COBALT AND COBALT BASE ALLOYS IN VACUUM TO 10-9 MILLIMETER OF MERCURY II-COBALT ALLOYS

NASA TN [D-132]

By Gorden, Sandford. NASA, Washington, D.C. 1959 . 161p , NASA Technical Notes D-131-140 Bounded Volumes Accession No. 63638; Contents: TR16036-44

Place Hold on NASA TN [D-132]

NASA TN [D-134]

By Weber,Richard J.. NASA, Washington, D.C. 1959 . 37p , NASA Technical Notes D-131-140 Bounded Volumes Accession No. 63638; Contents: TR16036-44

Place Hold on NASA TN [D-134]

NASA Technical Note [D-135]

By Kelly, Mark W.. NASA, Washington, D.C. 1959 . 37p , NASA Technical Notes D-131-140 Bounded Volumes Accession No. 63638; Contents: TR16036-44

Place Hold on NASA Technical Note [D-135]

NASA TN [D-136]

By Sultton, Fred B.. NASA, Washington, D.C. 1960 . 93p , NASA Technical Notes D-131-140 Bounded Volumes Accession No. 63638; Contents: TR16036-44

Place Hold on NASA TN [D-136]

NASA Technical Note [NASA TN D-381]: Free-spinning-tunnel investigation of a 1/20-scale model of an unswept-wing jet-propelled trainer airplane

Washington NASA 1960 . 18p , Bound together NASA TN D-381 to 390 | Bound vol. Acc. No. 63662 contains Acc. No. TR15585 to TR15589, TR15610, TR15590 to TR15591 & TR15611

Place Hold on NASA Technical Note [NASA TN D-381]: Free-spinning-tunnel investigation of a 1/20-scale model of an unswept-wing jet-propelled trainer airplane

NASA Technical Note [D-131]

By Rollbushler, R. James. NASA, Washington, D.C. 1959 . 16 , NASA Technical Notes D-131-140 Bounded Volumes Accession No. 63638; Contents: TR16036-44

Place Hold on NASA Technical Note [D-131]

Noise and wake structure measurement in a subsonic tip speed fan. [NASA CR-2323]

Washington, D. C NASA 1973 . 90p

Place Hold on Noise and wake structure measurement in a subsonic tip speed fan. [NASA CR-2323]

Flight evaluation of ground effect on several low-aspect-ratio airplanes.[NASA TN D-6053]

By Baker, A. Paul. Washington, D. C. NASA 1970 . 46p

Place Hold on Flight evaluation of ground effect on several low-aspect-ratio airplanes.[NASA TN D-6053]

Effects of reynolds number and model support on the supersonic aerodynamic characteristics of a 140 degree included angle cone [NASA TM X-3019]

By Trescot, Charles D.. Washington, D.C. National Aeronautics and Space Administration 1974 . 72p

Place Hold on Effects of reynolds number and model support on the supersonic aerodynamic characteristics of a 140 degree included angle cone [NASA TM X-3019]

Low Speed static longitudinal and lateral aerodynamic characteristics of a model with a low aspect ratio variable incidence wing and with a fre3e floating and a programed high lift canard control ( NASA TN D-1381)

By Scallion, William I.. Washington National Aeronautics and Space Administration 1962 . 64p

Place Hold on Low Speed static longitudinal and lateral aerodynamic characteristics of a model with a low aspect ratio variable incidence wing and with a fre3e floating and a programed high lift canard control ( NASA TN D-1381)

Effectas of lee surface volume addition on longitudinal aerodynamics of a high lift drag ratio wing body configuration an mach 6.0 [NASA TN D-4361

Washington, D. C. National Aeronautics and Space Administration

Place Hold on Effectas of lee surface volume addition on longitudinal aerodynamics of a high lift drag ratio wing body configuration an mach 6.0 [NASA TN D-4361

Supersonic aerodynamic characteristics of a series of related bodies with cross-sectional ellipticity [NASA TN D-3539]

By Fournier, Roger H. Washington, D.C. National aeronautics and Space Administration 1966 . 58p

Place Hold on Supersonic aerodynamic characteristics of a series of related bodies with cross-sectional ellipticity [NASA TN D-3539]

Use of tetrafluromethane to simulate real gas effects on the hypersonic aerodynamics of blunt vehicles [NASA TR R-312]

By Jones, Robert A.. Washington, D. C. National Aeronautics and Space Administration 1969 . 131p

Place Hold on Use of tetrafluromethane to simulate real gas effects on the hypersonic aerodynamics of blunt vehicles [NASA TR R-312]

Application of a one-srip integral method to tthe unsteady supersonic aerodynamics of an inclined flat surface [NASA TN D-6644]

By Bennet, Robert M.. Washington, D. C National Aeronautics and Space Administration 1972 . 55p

Place Hold on Application of a one-srip integral method to tthe unsteady supersonic aerodynamics of an inclined flat surface [NASA TN D-6644]

Aerodaynamics size distribution of suspanded particulate matter in the ambient air in the city of cleveland, ohio [NASA TM X-3124]

By Leibcki, Harold F.. Washington, D. C. National Aeronautics and Space Administration 1974 . 14p

Place Hold on Aerodaynamics size distribution of suspanded particulate matter in the ambient air in the city of cleveland, ohio [NASA TM X-3124]

Experimental aerodynamics characteristics for a cylindrical body of revolution with side strakes and varuious noses at angles of attack from 0 degree to 58 degree and mach numbers from 0.6 to 2.0 [NASA TM X-3130]

By Jorgensen, Leland H.. Washington, D. C. National Aeronautics and and Space Administration 1975 . 85p

Place Hold on Experimental aerodynamics characteristics for a cylindrical body of revolution with side strakes and varuious noses at angles of attack from 0 degree to 58 degree and mach numbers from 0.6 to 2.0 [NASA TM X-3130]

NASA Technical Note [D-2911-20]

Washington National Aeronautics and Space Administration (NASA) 1965 . 16p , NASA TN D-2911: Television tests with the syncom II synchronous communications satellite by Varice F. Henry and Michael E. McDonald | NASA TN D-2912: Two-step process to increase atomic hydrogen ION production in low-pressure radiofrequency discharge | NASA TN D-2913: experimental investigation of liquid impact in a model propellant tank | NASA TN D-2914: effects of wing dihedral and planform on stability characteristics of a research model at mach numbers from 1.80 to 4.63 | NASA TN D-2915: a long-life thermal cell | NASA TN D-2916: low power, low-level analog-to-digital converter for space vehicle applications | NASA TN D-2917 : the determination of absolute photon fluxes and applications to laboratory calibration procedures in the 100A to 300A range | NASA TN D-2918: visual presentation of the motion and oerietation of an orbiting spacecraft (OGO) | NASA TN D-2919: effect of electron radiation on TV lens componets | NASA TN D-2920: higher order approximation of runge-kutta type

Place Hold on NASA Technical Note [D-2911-20]

NASA Technical Note D-604

By Holl, Herbert B.. Washington National Aeronautics and Space Administration (NASA) 1961 . 53p , NASA Technical Note D-604

Place Hold on NASA Technical Note D-604

NASA Technical Translation [F-755]

Washington National Aeronautics and Space Administration (NASA) 1973 . 237p , Bounded Volumes Accession No. 101415 TR 10904 TR 10905 TT F-754-56

Place Hold on NASA Technical Translation [F-755]

NASA Technical Note [NASA TN D-3021]: Flight determined low-speed lift and drag characteristics of the lightweight M2-F1 lifting body

Washington NASA 1965 . 42p , Bound together NASA TN D-3021 to 3030 | Bound vol. Acc. No. 64302 contains Acc. No. TR10442 to TR10450

Place Hold on NASA Technical Note [NASA TN D-3021]: Flight determined low-speed lift and drag characteristics of the lightweight M2-F1 lifting body

NASA Technical Report [R- 31-40]

Washington NASA 1959 , NASA TR R-31 -- Analysis of turbulent flow and heat transfer in noncircular passages/ by Robert G. Deissler and Maynard F. Taylor | NASA TR R-32 -- Tables of the Bessel-Kelvin functions ber, bei, ker, kei, and their derivatives for the argument range 0(0.01)107.50/ by Herman H. Lowell | NASA TR R-33 -- Design of axisymmetric exhaust nozzles by method of characteristics incorporating a variable isentropic exponent/ by Eleanor Costilow Guentert and Harvey E. Neumann | NASA TR R-34 -- On fully developed channel flows: some solutions and limitations and effects of compressibility, variable properties and body forces/ by Stephen H. Maslen | NASA TR R-35 -- Ground reflection of jet noise/ by Walton L. Howes | NASA TR R-36 -- Two-dimensional diffusion theory analysis of reactivity effects of a fuel-plate-removal experiment/ by Edward R. Gotsky, James P. Cusick and Donald Bogart | NASA TR R-37 -- Boundary-layer stability diagrams for electrically conducting fluids in the presence of a magnetic field/ by Vernon J. Rossow | NASA TR R-38 -- The theory of diffusion in strained systems/ by Louis A. Girifalco and Hubert H. Grimes | NASA TR R-39 -- The phenomenon of change in buckle pattern in elastic structures/ by Manuel Stein | NASA TR R-40 -- Loads and deformations of buckled rectangular plates/ by Manuel Stein

Place Hold on NASA Technical Report [R- 31-40]

NASA Technical Note [D- 3811-20]

Washington NASA 1967 , NASA TN D-3811 -- Variations in gage constant as a function of emission current in an unshielded open-end grid bayard-alpert ionization gage/ by Leonard T. Melfi and Frederick A. Kern | NASA TN D-3812 -- Effect of thermocouple wire size and configuration on internal temperature measurements in a charring ablator/ by William D. Brewer | NASA TN D-3813 -- Interpretation of (d, α) reactions on fluorine 19 and nitrogen 15/ by Joseph R. Priest and John S. Vincent | NASA TN D-3814 -- Second Unites States manned three-pass orbital mission (Mercury-Atlas 7, spacecraft 18): description and performance analysis/ edited by John H. Boynton | NASA TN D-3815 -- Scalar and component wind correlations between altitude levels for Cape Kennedy, Florida, and Santa Monica, California/ by Glenn E. Daniels and Orvel E. Smith | NASA TN D-3816 -- Ionic conductivity of calcium and strontium fluorides/ by William L. Fielder | NASA TN D-3817 -- Ultrasonic attenuation in superconducting niobium/ by Joseph H. Simmons | NASA TN D-3818 -- Oxide-cathode durability in mercury electron-bombardment ion thrustor/ by William R. Kerslake | NASA TN D-3819 -- Cold-air performance evaluation of a scale-model fuel pump turbine for the M-1 hydrogen-oxygen rocket engine/ by Roy G. Stabe, John F. Kline and Edward H. Gibbs | NASA TN D-3820 -- Stress intensity factors for crackline-loaded edge-crack specimens/ by John E. Srawley and Bernard Gross

Place Hold on NASA Technical Note [D- 3811-20]

NASA Technical Report [NASA TR R-101]: Theoretical prediction of the effects of vortex flows on the loading, forces and moments of slender aircraft

Washington NASA 1961 . 102p , Bound together NASA TR R-101 to 105 | Bound vol. Acc. No. 65628 contains Acc. No. TR8433 to TR8436

Place Hold on NASA Technical Report [NASA TR R-101]: Theoretical prediction of the effects of vortex flows on the loading, forces and moments of slender aircraft

NASA TN [D-1096]

By Bandeen, W.R.. Washington National Aeronautics and Space Administration 1961 . 32p , Technical Note D-1091-99 Bound Vol. No.101065; Contents: TR16126-32

Place Hold on NASA TN [D-1096]

NASA TN [D-1097]

By Hempfling, Gerald L.. Washington National Aeronautics and Space Administration 1962 . 14p , Technical Note D-1091-99 Bound Vol. No.101065; Contents: TR16126-32

Place Hold on NASA TN [D-1097]

NASA TN [D-6552]

By Koenig, Robert W.. NASA, Washington, D.C. 1972 . 184p , NASA Technical Note D-6552,53,57,63,68 Bounded Volumes Accession No. 101251; Contents: TR13142-46

Place Hold on NASA TN [D-6552]

Aerodynamic charectristics in pitch of a 1/7 scale model of a two of a two and three stage rocket configuration at mach numbers of 0.4 to 4.63 [NASA TN D-5378]

By Hinson, William F.. Washington, D. C. National Aeronautics and Space Administration 1969 . 40p , Bound vol. contains NASA TN D 5371-5380

Place Hold on Aerodynamic charectristics in pitch of a 1/7 scale model of a two of a two and three stage rocket configuration at mach numbers of 0.4 to 4.63 [NASA TN D-5378]