Accession Number:

AD0641246

Title:

WIND TUNNEL INVESTIGATION OF AN ASPECT RATIO 10 TANDEM WING AIRCRAFT CONFIGURATION IN GROUND EFFECT. PART I. LONGITUDINAL CHARACTERISTICS

Personal Author(s):

Corporate Author:

DAVID TAYLOR MODEL BASIN WASHINGTON DC AERODYNAMICS LAB

Report Date:

1966-07-01

Abstract:

Subsonic wind-tunnel test results of a tandem wing aircraft configuration are given. Conventional longitudinal tests out of ground effect, and similar tests in ground effect, employing the ground board test technique, were conducted on the configuration. Test variables included height above the surface, forward and aft wing incidence angles, angle of attack, and center-of- gravity location. Author

Supplementary Note:

Bureau of Naval Weapons (Problem Assignment 1-34-52). DOI: 10.21236/AD0641246

Pages:

0071

Descriptors:

Subject Categories:

Communities Of Interest:

Distribution Statement:

Approved for public release; distribution is unlimited.

File Size:

3.87MB

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