Aerodynamics of a Rectangular Wing with a Peripheral Jet for Air Cushion Take-Off and Landing

Item

Title
Aerodynamics of a Rectangular Wing with a Peripheral Jet for Air Cushion Take-Off and Landing
Date
1965
Index Abstract
Coming Soon
Photo Quality
Complete
Report Number
AFFDL TR 65-59
Creator
Dau, K.
Etkin, B.
Surry, D.
Corporate Author
University of Toronto
Laboratory
Air Force Flight Dynamics Laboratory
Extent
56
Identifier
AD0623827
Access Rights
Notice(s)
Distribution Classification
1
Contract
AF 33(657)-8451
DoD Project
8219
DoD Task
821907
DTIC Record Exists
Yes
Distribution Change Authority Correspondence
None
Date Modified
Scanned by request 10/6/2006 submitted by a Private Citizen (No Known Affiliation)
Abstract
Subsonic wind tunnel experiments on a GETOL wing are reported. The main results relevant to performance, stability and control are presented, and applied to a hypothetical vehicle. Short-field capability is demonstrated to be possible. Stability and control problems are analysed, and shown not to be prohibitive.
Report Availability
Full text available
Date Issued
1965-09
Provenance
AFRL/VACA
Type
report
Format
1 online resource