Accession Number:

AD0698834

Title:

NUMERICAL PROGRAM AND EXAMPLES FOR DIFFRACTION OF SHOCK BY WINGS,

Descriptive Note:

Corporate Author:

NEW YORK UNIV BRONX DEPT OF AERONAUTICS AND ASTRONAUTICS

Personal Author(s):

Report Date:

1969-04-01

Pagination or Media Count:

82.0

Abstract:

The paper is intended to be a supplement for and should be used in conjunction with Diffraction of Shock Wave by Moving Thin Wing, L. Ting and M. Gunzburger, AFOSR-69-2814 TR. The numerical program used to determine the pressure is listed and various aspects of it are discussed. An extensive number of examples are given for the pressure on simple and composite symmetric thin wings. The lift on simple triangular wings with supersonic leading edges is also determined. Author

Subject Categories:

  • Aerodynamics
  • Aircraft
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE