Accession Number : AD0846423

Title :   Research and Exploratory Development for the Office of Aeronautical Research, National Aeronautics and Space Administration.

Descriptive Note : Quarterly progress rept. Jul-Sep 68,

Corporate Author : JOHNS HOPKINS UNIV LAUREL MD APPLIED PHYSICS LAB

Personal Author(s) : Wagner, J. P. ; Rice, J. L. ; Billig, F. S. ; Yates, C. L. ; Schetz, J. A.

Report Date : SEP 1968

Pagination or Media Count : 13

Abstract : The objective of this research is to determine some of the design criteria and the expected performance of the combustor and nozzle for hypersonic ramjets with supersonic combustion of hydrogen in the flight Mach number range from 5 to at least 10. (Author)

Descriptors :   (*SUPERSONIC COMBUSTION, ABSTRACTS), SUPERSONIC COMBUSTION RAMJET ENGINES, HYPERSONIC NOZZLES, HYDROGEN, TURBULENCE, JET MIXING FLOW, NOZZLE GAS FLOW, TWO DIMENSIONAL FLOW, HYPERSONIC CHARACTERISTICS.

Subject Categories : Fluid Mechanics
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE