Accession Number:

ADA066968

Title:

Supersonic Flow Past Two Intersecting and Two Parallel Wings,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1978-06-21

Pagination or Media Count:

27.0

Abstract:

Subject Categories:

  • Aircraft
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE