Accession Number:

ADA066477

Title:

Experimental Study of the Supersonic Flow Around V-Shaped Wings,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1978-08-09

Pagination or Media Count:

30.0

Abstract:

Subject Categories:

  • Aircraft
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE