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National Advisory Committee for Aeronautics Collection
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National Advisory Committee for Aeronautics Collection
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Flight tests of thermal ice-prevention equipment in the XB-24F airplane
Comparison of the performance of a helicopter-type ram-jet engine under various centrifugal loadings
A Preliminary Investigation of the Performance of a Short Length Turbojet Combustor Using Vaporized Hydrocarbon Fuels
Wind-Tunnel Investigation at Low Speed of a Wing Having 63 Degree Sweepback and a Drooped Tip
Flight measurements of directional stability to a Mach number of 1.48 for an airplane tested with three different vertical tail configurations
A variable-geometry axisymmetric supersonic inlet with telescoping centerbody
Performance of a short combustor at high altitudes using hydrogen fuel
Performance characteristics of axisymmetric two-cone and isentropic nose inlets at Mach number 1.90
Design and test of mixed-flow impellers 6: performance and parabolic-bladed impeller with shroud redesigned by rapid approximate method
A theoretical analysis of the effect of engine angular momentum on longitudinal and directional stability in steady rolling maneuvers
Analytical comparison of convection-cooled turbine blade cooling-air requirements for several radial gas-temperature profiles
Propagation of a free flame in a turbulent gas stream
Speed-Brake Investigation at Low Speed of a 1/10-Scale Model of the MX-1554A Airplane With a Circular Jet Nozzle
Minimum Drag of Four Versions of a Swept-Wing Fighter Airplane Obtained From Flight Tests of Rocket-Boosted Models at Mach Numbers From 0.81 to 1.71
Wind-Tunnel Investigation at Low Speed of the Rolling Stability Derivatives of a 1/10-Scale Model of the Douglas A4D-1 Airplane
A Low-Pressure-Loss Short Afterburner for Sea-Level Thrust Augmentation
Measurements of Pressure Drop with No Heat Addition on Mockup Segments of the General Electric Air-Cooled Aircraft Reactor
Wind-Tunnel Investigation of the Aerodynamic Characteristics of a 0.07-Scale Model of the North American MX-770 Missile
Some Effects of Reynolds Number on the Stability of a Series of Flared-Body and Blunted-Cone Models at Mach Numbers From 1.62 to 6.86
Performance of Multiple Jet-Exit Installations
Brief Studies of Turbojet Combustor and Fuel-System Operation With Hydrogen Fuel at -400 Degrees F
Flight Investigation of a Roll-Stabilized Ramjet Test Vehicle Over a Mach Number Range of 2.3 to 2.7
Static Stability and Control of Hypersonic Gliders
An Investigation of the Performance of a Semielliptical Scoop Inlet at Mach Numbers of 1.60, 1.76, and 2.02
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