NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
The augmentor wing - Powered-lift STOL a proven conceptA jet-STOL powered-lift aircraft has the ability to perform a relatively steep (7.5 deg) final approach at high power setting and a low speed. The DHC-5 Buffalo/Spey Augmentor-Wing research aircraft is the first machine of its kind to accomplish this performance. The aircraft uses an approach in which the cold bypass thrust is vectored by the augmentor flap. Aspects of aircraft reliability are discussed together with taxi trials, stalling characteristics, lateral directional control, single-engine operations, roll acceleration, and flight in turbulent conditions.
Document ID
19740038978
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Whittley, D. C.
(Havilland Aircraft of Canada, Ltd. Downsview, Ontario, Canada)
Date Acquired
August 7, 2013
Publication Date
February 1, 1974
Publication Information
Publication: Interavia
Volume: 29
Subject Category
Aircraft
Accession Number
74A21728
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available