Accession Number:

AD0631313

Title:

ON THE DETERMINATION OF OPTIMUM SUPERSONIC THRUST NOZZLES OF GIVEN LENGTH FOR A FLOW WITH SWIRL: THEORETICAL PART.

Descriptive Note:

Scientific rept.,

Corporate Author:

AEROSPACE RESEARCH LABS OFFICE OF AEROSPACE RESEARCH WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1966-01-01

Pagination or Media Count:

46.0

Abstract:

The problem of maximizing the thrust in supersonic nozzles of given length has been treated previously by Guderley and Rao. Significant differences of the nozzle shapes may be encountered if the oncoming flow possesses a swirl around the axis of symmetry. The present paper extends the existing theory to this case. The final procedure turns out to be more complex, but the basic considerations carry over to the present case. Some space has been devoted to a discussion of a short cut by which Rao succeeded in by-passing the characteristic conditions. The report contains the basic theory only. Author

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE