Accession Number:

ADA065993

Title:

Supersonic Flow in the Area of Antisymmetric Thin Cruciform Wings with Supersonic Leading Edges in a Horizontal Plane, with Consideration of Flow Separation on the Edges,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1978-10-30

Pagination or Media Count:

19.0

Abstract:

Subject Categories:

  • Aircraft
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE