Accession Number:

AD0750950

Title:

Reduction of Base Drag during Supersonic Velocities using Power Method,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1972-09-07

Pagination or Media Count:

8.0

Abstract:

The article describes the results of experimental drag investigation of a nacelle containing two engines and a wing of a long range supersonic plane for M 2.4.

Subject Categories:

  • Aircraft
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE