Accession Number:

ADA065992

Title:

Theory of Thin Wing in a Supersonic Flow with Consideration of the Non-Equilibrium State of Excitation of Oscillating Degrees of Freedom,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1978-11-09

Pagination or Media Count:

18.0

Abstract:

Subject Categories:

  • Aircraft
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE