NASA Technical Reports Server (NTRS) : Evaluation pdf

NASA Technical Reports Server (NTRS) : Evaluation

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Description of the Book:

The potential performance of oblique detonation wave ramjets is analyzed in terms of multishock diffusion, oblique detonation waves, and heat release. Results are presented in terms of thrust coefficients and specific impulses for a range of flight Mach numbers of 6 to 16

• Creator/s: NASA Technical Reports Server (NTRS
• Date: 1/1/1978
• Year: 1978
• Book Topics/Themes: NASA Technical Reports Server (NTRS), DETONATION WAVES, EVALUATION, OBLIQUE SHOCK WAVES, RAMJET ENGINES, HYPERSONIC FLIGHT, PERFORMANCE TESTS, THRUST MEASUREMENT, Morrison, R. B

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