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High-Speed Measurements on a Swept-Back Wing (Sweepback Angle phi = 35 Deg)In the following, high-speed measurements on a swept-back wing are reported. The curves of lift, moment, and drag have been determined up to Mach numbers of M = 0.87, and they are compared to a rectangular wing. Through measurements of the total-head loss behind the wing and through schlieren pictures, an insight into the formation of the compression shock at high Mach numbers has been obtained.
Document ID
20050019388
Acquisition Source
Langley Research Center
Document Type
Other - NACA Technical Memorandum
Authors
Goethert, B.
Date Acquired
August 22, 2013
Publication Date
March 1, 1947
Publication Information
Publication: Lilienthal-Gesellschaft fuer Luftfahrtforschung
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NACA-TM-1102
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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