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Wind-Tunnel Investigations on a Changed Mustang Profile with Nose Flap Force and Pressure-Distribution MeasurementsMeasurements are described which were taken in the large wind tunnel of the AVA on a rectangular wing "Mustang 2" with nose flap of a chord of 10 percent. Besides force measurements the results of pressure-distribution measurements are given and compared with those on the same profile "without" nose flap.
Document ID
20050031128
Acquisition Source
Langley Research Center
Document Type
Other - NACA Technical Memorandum
Authors
Krueger, W. (Zentrale fuer Wissenschaftliches Berichtswesen Berlin, Germany)
Date Acquired
August 22, 2013
Publication Date
September 1, 1947
Publication Information
Publication: Untersuchungen und Mitteilungen
Issue: 3153
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NACA-TM-1177
Report Number: NACA-TM-1177
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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