Transonic and supersonic ejection release characteristics of six dynamically scaled external-store shapes from an 0.086-scale model of a current fighter airplane
Fighter aircraft external stores ejection at transonic and supersonic speeds
EJECTION↗
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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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Cold-air performance evaluation of scale model oxidizer pump-drive turbine for the M-1 hydrogen-oxygen rocket engine. II - Overall two-stage performance
Cold flow test of pump drive turbines for M-1 rocket engine
M-1 ROCKET ENGINE↗
Investigation of the subsonic and supersonic release characteristics of an externally carried fuel tank from a 1/4 d-scale model of a bomber airplane
Release and flight characteristics study for externally carried fuel tank models of various configurations at subsonic and supersonic speeds
FLIGHT CHARACTERISTICS↗
Effects of vertical-tail size and a ventral fin on the static lateral and directional stability derivatives of a 0.048-scale model of a horizontal-attitude VTOL airplane at transonic speeds
Vertical tail size and ventral fin effects on lateral and directional stability of VTOL AIRCRAFT at transonic speeds
VTOL AIRCRAFT↗
Aerodynamic characteristics in pitch, including effects of horizontal-tail negative dihedral angle, of a 0.048-scale model of a horizontal-attitude VTOL airplane at transonic speeds
Aerodynamic characteristics in pitch of horizontal attitude VTOL aircraft, including effects of negative dihedral horizontal tail
PITCHING MOMENT↗
Low-speed tests of 50 deg-swept parawings applied to a 0.17-scale model of a manned flight vehicle
Shock wave interference and degradation in wind tunnel caused by protruding teeth, recessions, local expansions, and combinations of these
SWEPT WING↗
Hypersonic static stability investigation of a Tomahawk 20-percent-scale model Technical report, 27 May - 2 Jun. 1966
Hypersonic static stability investigation of Tomahawk rocket model
HYPERSONIC FLOW↗
Scale model study of flow patterns in the inlet manifold of the fuel pump drive turbine for the M-1 hydrogen-oxygen rocket engine
Flow conditions in inlet manifold of M-1 fuel pump drive turbine investigated using circumferential static pressure measurements in conjunction with smoke trace photographs
Kline, J. F.↗
Static and dynamic longitudinal stability derivatives of a powered 0.18-scale model of a fan-in-wing VTOL aircraft
Static and dynamic longitudinal stability tests of fan in wing V/STOL aircraft model
Chambers, J. R.↗
Spectral radiance measurements of exhaust plumes from scale model rocket engines.
Spectral radiance of rocket exhaust plumes at high altitudes
Mccaa, D. J.↗
Static stability characteristics of a 0.16- scale model of a jet-lift V/STOL research airplane in cruise
Wind tunnel investigation of static stability characteristics of model jet-lift V/STOL research airplane
Winston, M. M.↗
Effect of hypersonic research engine installation on aerodynamic characteristics of 0.0667-scale model of X-15A-2 airplane at Mach numbers from 1.75 to 4.63
Wind tunnel stability tests to determine effect of hypersonic research engine on aerodynamic characteristics of research aircraft
Graves, E. B.↗
Thermal scale modeling of a spacecraft radiator with coupled forced convection- conduction-radiation heat transfer Annual report
Design and development of spacecraft radiator using forced convection, conduction, and radiation for heat transfer under steady state conditions
Colvin, D. P.↗
Effects of free-stream Reynolds number, engine installation, and model scale on stability characteristics of a translating- spike inlet at Mach 2.0
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Bowditch, D.↗
Wind-Tunnel Investigation of a 0.6-Scale Model of Hughes MX-904 Tail Surface at Supersonic Speeds. Tail Attached to a Segment of the Foreshortened Body
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Conner, D. W.↗
Wind-Tunnel Investigation of the Aerodynamic Characteristics of a 0.07-Scale Model of the North American MX-770 Missile
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Pfyl, F. A.↗
Investigation of a 1/4 Scale Model of the Republic F-105 Airplane in the Langley 19 Foot Pressure Tunnel. Longitudinal Stability and Control and Horizontal-Tail Hinge-Moment and Normal-Force Characteristics of the Model Equipped with a Drooped Supersonic-Type Elliptical Wing-Root Inlet
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Cancro, P. A.↗
Experimental investigation at high subsonic speeds of the rolling-stability derivatives of a 1/22 scale model of the Republic F-105 airplane
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Hayes, W. C., Jr.↗