Accession Number:

ADA063773

Title:

The Utilization of the Analytic Graph Method to Determine the Best Shape of Thin Delta Wings in Supersonic Flow,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Report Date:

1978-06-29

Pagination or Media Count:

20.0

Abstract:

Subject Categories:

  • Aircraft
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE