Accession Number:

AD0645641

Title:

RESEARCH STUDY TO VERIFY AND EXTEND HIGH SPEED MATH MODEL FOR JET REACTION CONTROL EFFECTIVENESS.

Descriptive Note:

Final rept.,

Corporate Author:

MARTIN CO ORLANDO FLA

Personal Author(s):

Report Date:

1966-08-01

Pagination or Media Count:

121.0

Abstract:

An analytical model was developed to predict the performance of a two-dimensional, reaction control jet exhausting normal to supersonic and hypersonic streams. The separation of a turbulent boundary layer upstream of the jet and the pressure field downstream of the jet were studied. A wind tunnel test of a jet slot on a flat plate model was conducted. The existing flow model was revised to give improved accuracy of the predictions of the interference effects upstream of the jet. The flow model was extended to include interference effects downstream of the jet. Author

Subject Categories:

  • Aircraft
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE