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Transonic Wind-Tunnel Test Of An Oblique WingReport describes transonic wind-tunnel tests of oblique, pivotable wing fitted to 0.087-scale model of F-8 airplane. Purpose of tests to study performance and stability characteristics. Conducted to determine whether placement of pivot at higher position above fuselage than previously results in less side force and yawing moment than observed in previous tests at low speeds.
Document ID
19920000759
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Kennelly, R. A. (NASA Ames Research Center, Moffett Field, CA.)
Strong, J. M. (NASA Ames Research Center, Moffett Field, CA.)
Carmichael, R. L. (NASA Ames Research Center, Moffett Field, CA.)
Kroo, I. M. (Stanford Univ.)
Date Acquired
August 15, 2013
Publication Date
December 1, 1992
Publication Information
Publication: NASA Tech Briefs
Volume: 16
Issue: 12
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
ARC-12812
Accession Number
92B10759
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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