Accession Number:

AD0766641

Title:

STOL Tactical Aircraft Investigation. Volume IV. Analysis of Wind Tunnel Data: Vectored Thrust/Mechanical Flaps and Internally Blown Jet Flaps

Descriptive Note:

Final technical rept. 8 Jun 1971-8 Dec 1972

Corporate Author:

BOEING AEROSPACE CO SEATTLE WA

Report Date:

1973-05-01

Pagination or Media Count:

304.0

Abstract:

The report presents the analysis of 728 hours of testing, conducted in the Boeing VSTOL 20 x 20 ft. Wind Tunnel, on a model of a medium STOL transport with vectored thrust and jet flap powered-lift systems. The interactions between the two powered lift systems and the basic airplane aerodynamics are presented for a systematic series of configuration changes which include sweep and nacelle location.

Subject Categories:

  • VSTOL

Distribution Statement:

APPROVED FOR PUBLIC RELEASE