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

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