Accession Number:

AD0747408

Title:

A Circular Cone under an Angle of Attack in a Supersonic Flow of Gas,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1972-05-26

Pagination or Media Count:

17.0

Abstract:

An investigation is reported of the flow around a cone at a small angle of attack by a uniform supersonic flow of an ideal gas. The problem is solved by the method of small disturbances. The present work presents a solution in the eddy layer with favorable accuracy. The desired solution is reduced in the work to quadratures. Author

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE