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Comparison of Drop and Wind-Tunnel Experiments on Bomb Drag at High Subsonic SpeedsThe drag coefficients of bombs at high velocities velocity of fall was 97 percent of the speed of sound) (the highest are determined by drop tests and compared with measurements taken in the DVL high-speed closed wind tunnel and the open jet at AVA - Gottingen.
Document ID
20050019654
Acquisition Source
Langley Research Center
Document Type
Other - NACA Technical Memorandum
Authors
Gothert, B. (Zentrale fuer Wissenschaftliches Berichtswesen Berlin, Germany)
Date Acquired
August 22, 2013
Publication Date
May 1, 1948
Publication Information
Publication: Deutsche Luftfahrtforschung Forschungsbericht
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NACA-TM-1186
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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