Accession Number:

ADA067323

Title:

High Angle of Attack Aerodynamics

Descriptive Note:

Conference proceedings

Corporate Author:

ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT NEUILLY-SUR-SEINE (FRANCE)

Personal Author(s):

Report Date:

1979-01-01

Pagination or Media Count:

550.0

Abstract:

The Symposium was organized because of the continuing need for design data and principles relevant to the flight of aircraft and missiles at high angles of attack and the substantial efforts devoted to vehicles capable of controlled flight in that regime. Four sessions were held on 1 Studies of Configurations of Practical Application 10 Papers 2 Mathematical Modelling and Supporting Investigations 12 Papers 3 Design Methods 7 Papers, and 4 Air Intakes 2 Papers. Eight additional short presentations on these subjects are also documented. A Round Table Discussion on the state-of-art and recommendations for continuing effort in high-angle-of-attack aerodynamics is also documented in the report.

Subject Categories:

  • Aircraft
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE