A pressure-distribution investigation of a supersonic-aircraft fuselage and calibration of the Mach number 1.40 nozzle of the Langley 4- by 4-foot supersonic tunnel
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Hasel, Lowell E↗
SEARCH · Engineering Papers
Results for “Supersonics”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Langley 9-inch Supersonic Tunnel Tests of Several Modifications of a Supersonic Missile Having Tandem Cruciform Lifting Surfaces : Three-component Data Results of Models Having Ratios of Wing Span to Tail Span Equal to and Less than 1 and Some Static
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Rainey, Robert W↗
Langley 9-inch Supersonic Tunnel Tests of Several Modifications of a Supersonic Missile Having Tandem Cruciform Lifting Surfaces : Three-component Data Results of Models Having Ratios of Wing Span to Tail Span Equal to 1
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Rainey, Robert W↗
Langley 9-inch supersonic tunnel tests of several modifications of a supersonic missile having tandem cruciform lifting surfaces : three-component data results of models having ratios of wing span to tail span less than 1
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Rainey, Robert W↗
Application of Supersonic Vortex-flow Theory to the Design of Supersonic Impulse Compressor- or Turbine-blade Sections
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Wlodarski, John↗
Subsonic and supersonic hinge-moment and effectiveness characteristics of an unbalanced lateral control having low theoretical hinge moments at supersonic speeds
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Goin, Kennith L↗
Some Studies of Axisymmetric Free Jets Exhausting from Sonic and Supersonic Nozzles into Still Air and into Supersonic Streams
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Love, Eugene S↗
Investigation of the effects of model scale and stream Reynolds number on the aerodynamic characteristics of two rectangular wings at supersonic speeds in the Langley 9-inch supersonic tunnel
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Coletti, Donald E↗
Initial inclination of the mixing boundary separating an exhausting supersonic jet from a supersonic ambient stream
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Love, Eugene S↗
Investigation of fixed-geometry supersonic inlets with bypass ducts for matching turbojet-engine air-flow requirements over a range of transonic and supersonic speeds
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Leiss, Abraham↗
Preliminary investigation of effects of combustion in ram jet performance of supersonic diffusers II : perforated supersonic inlet
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Schroeder, Albert H↗
Low Density Supersonic Decelerator (LDSD) Supersonic Flight Dynamics Test (SFDT) Plume Induced Environments Modelling
No abstract available
Mobley, Brandon↗
First Test Flight Thermal Performance of the Low Density Supersonic Decelerator (LDSD) Supersonic Flight Dynamics Test (SFDT) Vehicle
The thermal telemetry from the first test flight, an assessment of post-flight inspections of the recovered vehicle, and a review of the thermal design and model of the vehicle will be presented along with several lessons learned.
flight test data↗
Low Density Supersonic Decelerators (LDSD): Reconstructed Parachute System Performance During the Second Supersonic Flight Dynamics Test
No abstract available
O'Farrell, Clara↗
Supercomputing in Supersonics: Quiet Supersonic Flight
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CST↗
The Supersonic Project: To Cool or Not to Cool Supersonically Induced Gas Objects (SIGOs)?
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Yeou S. Chiou↗