Accession Number:

ADA045073

Title:

Investigation of Velocity Field Behind Low-Flying Wing with Fuselage,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1977-05-11

Pagination or Media Count:

21.0

Abstract:

This article proposes a method for investigation of the velocity field behind a low-flying wing with fuselage. The value of the velocity field is necessary in calculating the aerodynamic characteristics of the tail assembly of aircraft which use the screen effect.

Subject Categories:

  • Aerodynamics
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE