The progress report for the grant entitled 'Hypervelocity of Scramjet Combustor-Nozzle Analysis and Design' is presented. The three main tasks in the program are combustor modeling study, development of anaylsis capabilities for hypersonic scramjet nozzles, and development of optimum design methods for hypersonic scramjet nozzles. The research performed was documented in a series of technical publications and presentations at various conferences. A brief description of the research in each of the above three areas and a list of the resulting technical publications are included.
Hypervelocity Scramjet Combustor-Nozzle Analysis and Design
1992
6 pages
Report
Keine Angabe
Englisch
Jet & Gas Turbine Engines , Aerodynamics , Aircraft , Computational fluid dynamics , Design analysis , Hypersonic nozzles , Hypervelocity , Nozzle design , Supersonic combustion ramjet engines , Combustion chambers , Nozzle flow , Jet thrust , Nozzle geometry , Optimization , Performance prediction , Steady flow , Supersonic combustion , Two dimensional models
Scramjet Combustor and Nozzle Computations
British Library Online Contents | 1992
|Numerical Study of Hypervelocity Flows Through a Scramjet Combustor
Online Contents | 1997
|A Numerical Study of Hypervelocity Flows Through a Scramjet Combustor
British Library Conference Proceedings | 1994
|