Publication Date:
2019-08-16
Description:
The experimentally determined interaction effects of a side jet exhausting near the base of an ogive-cylinder model are presented and discussed. The interaction force appears to be independent of main-stream Mach number, boundary-layer condition (laminar or turbulent), angle of attack, and forebody length. The ratio of interaction force to jet force is found to be inversely proportional to the square root of the product of jet stagnation-to-free-stream pressure ratio and jet-to-body diameter ratio.
Keywords:
Fluid Mechanics and Heat Transfer
Type:
NASA-MEMO-12-5-58W
Format:
application/pdf