Accession Number:

ADA003955

Title:

An Experimental Investigation of the Effect of a Fuselage on Wing Characteristics.

Descriptive Note:

Final rept. 1 Apr 64-31 Mar 68,

Corporate Author:

PRINCETON UNIV N J DEPT OF AEROSPACE AND MECHANICAL SCIENCES

Personal Author(s):

Report Date:

1975-01-01

Pagination or Media Count:

212.0

Abstract:

A series of experimental investigations utilizing flow visualization, force measurement and pressure distribution techniques to investigate the effect on wing lift of fuselage placement and cross-sectional shape are reported. Emphasis is placed on conditions involving large circulation including the use of circulation control.

Subject Categories:

  • Aerodynamics
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE