Suggested Topics within your search.
Suggested Topics within your search.
- Airplanes 50
- Mathematical models 34
- Testing 25
- Heat 21
- Transmission 20
- Aerodynamics 18
- Aerodynamics, Supersonic 18
- Measurement 15
- Wings, Swept-back 14
- Aerodynamic load 13
- Boundary layer 13
- Aerodynamics, Transonic 11
- Turbulence 10
- Aerodynamic heating 8
- Drag (Aerodynamics) 8
- Rotors (Helicopters) 8
- Fatigue 7
- Space vehicles 7
- Turbulent boundary layer 7
- Wings 7
- Combustion 6
- Mach number 6
- Rocket engines 6
- Rockets (Aeronautics) 6
- Thermal properties 6
- Wind tunnel testing 6
- Angle of attack (Aerodynamics) 5
- Blades 5
- Lift (Aerodynamics) 5
- Materials 5
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141
Comparison of measured flapwise structural bending moments on a teetering rotor blade with results calculated from the measured pressure distribution /
Published 1959“…NASA memorandum ;…”
Government Document Book -
142
Details of exact low Prandtl number boundary-layer solutions for forced and for free convection /
Published 1959“…NASA memorandum ;…”
Government Document Book -
143
Effect of ozone addition on combustion efficiency of hydrogen-liquid-oxygen propellant in small rockets /
Published 1959“…NASA memorandum ;…”
Government Document Book -
144
1958 NASA/USAF space probes (ABLE-1) final report.
Published 1959“…NASA memorandum ;…”
Government Document Book -
145
Investigation of the stability of very flat spins and analysis of effects of applying various moments utilizing the three moment equations of motion /
Published 1959“…NASA memorandum ;…”
Government Document Book -
146
A simple method for determining heat transfer, skin friction, and boundary-layer thickness for hypersonic laminar boundary-layer flows in a pressure gradient /
Published 1959“…NASA memorandum ;…”
Government Document Book -
147
Water-landing characteristics of a reentry capsule /
Published 1959“…NASA memorandum ;…”
Government Document Book -
148
A method for computing turbulent heat transfer in the presence of a streamwise pressure gradient for bodies in high-speed flow /
Published 1959“…NASA memorandum ;…”
Government Document Book -
149
Measurements of local heat transfer and pressure on six 2 inch diameter blunt bodies at a Mach number of 4.95 and at Reynolds numbers per foot up to 81 x 10⁶ /
Published 1959“…NASA memorandum ;…”
Government Document Book -
150
Estimated performance of radial-flow exit nozzles for air in chemical equilibrium /
Published 1959“…NASA memorandum ;…”
Government Document Book -
151
The effect of beam loading on water impact loads and motions /
Published 1959“…NASA memorandum ;…”
Government Document Book -
152
Analytical investigation of the significance of turbine-inlet temperature in high-energy rocket turbodrive applications /
Published 1959“…NASA memorandum ;…”
Government Document Book -
153
Pressure drag of axisymmetric cowls having large initial lip angles at mach numbers from 1.90 to 4.90 /
Published 1959“…NASA memorandum ;…”
Government Document Book -
154
A hydrogen peroxide hot-jet simulator for wind-tunnel tests of turbojet-exit models /
Published 1959“…NASA memorandum ;…”
Government Document Book -
155
Experimental investigation of aerodynamic effects of external combustion in airstream below two-dimensional supersonic wing at mach 2.5 and 3.0 /
Published 1959“…NASA memorandum ;…”
Government Document Book -
156
Combustion of various highly reactive fuels in a 3.84-by-10-inch mach 2 wind tunnel /
Published 1959“…NASA memorandum ;…”
Government Document Book -
157
A numerical method for calculating the wave drag of a configuration form the second derivative of the area distribution of a series of equivalent bodies of revolution /
Published 1959“…NASA memorandum ;…”
Government Document Book -
158
Semiempirical procedure for estimating lift and drag characteristics of propeller-wing-flap configurations for vertical-and short-take-off-and landing airplanes /
Published 1959“…NASA memorandum ;…”
Government Document Book -
159
Heat transfer in the turbulent incompressible boundary layer.
Published 1958“…NASA memorandum ;…”
Government Document Book -
160
A weight comparison of several attitude controls for satellites /
Published 1959“…NASA memorandum ;…”
Government Document Book