NASP X-30 Propulsion technology status [PDF]
The performance goals of the NASP program require an aero-propulsion system with a high effective specific impulse. In order to achieve these goals, the high potential performance of air-breathing engines must be achieved over a very wide Mach number ...
Powell, William E.
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Tunable Diode Laser Absorption Spectroscopy Based Temperature Measurement with a Single Diode Laser Near 1.4 μm. [PDF]
Sensors (Basel), 2022 Liu X, Ma Y.
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Exploratory study of transient upstart phenomena in a three-dimensional fixed-geometry scramjet engine [PDF]
The structural and thermal design of a hydrogen fueled regeneratively cooled three dimensional fixed geometry scramjet was examined. An exploratory study was conducted at Mach 5.3 in the 7-inch Mach 7 pilot tunnel to investigate the unstart phenomena and
Wieting, A. R.
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Thermal-structural design study of an airframe-integrated Scramjet [PDF]
The development and evaluation of a design concept for the cooled structures assembly for the Scramjet engine is discussed. Development concepts for engine subsystems and design concepts for the aircraft/engine interface are included.
Katinszky, E. A. +5 more
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Validation of scramjet exhaust simulation technique at Mach 6 [PDF]
Current design philosophy for hydrogen-fueled, scramjet-powered hypersonic aircraft results in configurations with strong couplings between the engine plume and vehicle aerodynamics.
Hopkins, H. B., Konopka, W., Leng, J.
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Secondary Flow Effect on Supercritical Kerosene Oxidation Deposition and Heat Transfer in a Coiled Tube. [PDF]
ACS Omega, 2022 Pei X, Tian H, Zheng Z, Wang Y, Hou L.
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Tuning Process for the Modified Magnussen Combustion Model [PDF]
In the application of CFD to turbulent reacting flows, one of the main limitations to predictive accuracy is the chemistry model. Using a full or skeletal kinetics model may provide good predictive ability, however, at considerable computational cost ...
Norris, A. T.
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Compendium of NASA Langley reports on hypersonic aerodynamics [PDF]
Reference is made to papers published by the Langley Research Center in various areas of hypersonic aerodynamics for the period 1950 to 1986. The research work was performed either in-house by the Center staff or by other personnel supported entirely or ...
Cary, Aubrey M. +2 more
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Shock tunnel studies of scramjet phenomena, supplement 6 [PDF]
Reports by the staff of the University of Queensland on various research studies related to the advancement of scramjet technology are presented.
Allen, G. +9 more
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A parametric study of effect of forebody shape on flow angularity at Mach 8 [PDF]
Flow angularity and static pressure measurements have been made on the lower surface of nine forebody models that simulate the bottom forward surface of a hypersonic aircraft. Measurements were made in an area of the forebody that represents the location
Johnson, C. B., Marcum, D. C., Jr.
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