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Evaluation of the oblique detonation wave ramjet
- Publication Year :
- 1978
- Publisher :
- United States: NASA Center for Aerospace Information (CASI), 1978.
-
Abstract
- 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.
- Subjects :
- Fluid Mechanics And Heat Transfer
Subjects
Details
- Language :
- English
- Database :
- NASA Technical Reports
- Notes :
- NAS1-14771
- Publication Type :
- Report
- Accession number :
- edsnas.19780017411
- Document Type :
- Report