Accession Number:

AD0787459

Title:

Review of Methods of Solution of Afterbody/Exhaust Nozzle Flow Fields,

Descriptive Note:

Corporate Author:

AIR FORCE FLIGHT DYNAMICS LAB WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1974-01-01

Pagination or Media Count:

165.0

Abstract:

A review is made of methods of solution for afterbodyexhaust nozzle flow fields in different flight regimes. For the transonic regime airfoil solutions are also presented. A comparison between various theories and experiments is made wherever considered necessary to show the state-of-the-art. Most of the available theories are selected and correlated. Author

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE