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

Download this report (PDF, 8.71 MB, 300 pages)
Report Number: AFFDL TR 73-19 Volume 4
Author(s): Monk, John R., Palmer, Patrick, Lee, Jerry E.
Corporate Author(s): The Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Corporate Report Number: D180-14411-1
Date of Publication: 1973-05
Pages: 300
Contract: F33615-71-C-1757
DoD Project: 643A
Identifier: AD0766641

Abstract:
The report presents the analysis of 728 hours of testing, conducted in the Boeing V/STOL 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.

Provenance: AFRL/VACA

Other options for obtaining this report:

Via the Defense Technical Information Center (DTIC):
A record for this report, and possibly a pdf download of the report, exists at DTIC

Via National Technical Report Library:
This report may be available for download from NTRL. Use the Title from this record to locate the item in DTIC Online

Indications of Public Availability
No digital image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement



Export