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Comparison of Experimental Thrust Measurements with Theoretical Values for a Scramjet Engine
12th AIAA International Space Planes and Hypersonic Systems and Technologies
◽
10.2514/6.2003-6961
◽
2003
◽
Cited By ~ 2
Author(s):
Judy Odam
◽
Allan Paull
Keyword(s):
Scramjet Engine
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Dynamic Computational Analyses of Complete Scramjet Engine Modules
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Inhomogeneous behavior of supercritical hydrocarbon fuel flow in a regenerative cooling channel for a scramjet engine
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Hydrocarbon Fuel
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Cooling Channel
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Regenerative Cooling
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Fuel Flow
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Design and analysis of an inlet and combustion chamber of scramjet engine
10.1063/5.0034510
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Nivin Joy
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Thermal analysis of a high-efficiency internally-cooled strut injector for scramjet engine
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W.Q. Li
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Thermal Analysis
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Development status of the NAL Ramjet Engine Test Facility and sub-scale scramjet engine
10.2514/6.1992-5094
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Test Facility
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Development Status
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Scramjet Engine
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Performance Characteristics of a Scramjet Engine at Mach 10 to 15 Flight Condition
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Scramjet Engine Performance Attained in RJTF Testing
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2004
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Influences of accelerating states on supercritical n-decane heat transfer in a horizontal tube applied for scramjet engine cooling
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Keyword(s):
Heat Transfer
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Horizontal Tube
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