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Flight Tests to Determine the Effect of Length of a Conical Windshield on the Drag of a Bluff Body at Supersonic SpeedsFlight tests were conducted to determine the effect of length of a conical windshield on the drag of a bluff body moving at supersonic speeds. A comparison is made between results obtained and results of previous drag tests of body-windshield combinations.The effect of increasing the length of the windshield is discussed.
Document ID
20030064196
Acquisition Source
Langley Research Center
Document Type
Other - NACA Research Memorandum
Authors
Alexander, Sidney R. (National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Katz, Ellis (National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Date Acquired
September 7, 2013
Publication Date
January 29, 1947
Subject Category
Aerodynamics
Report/Patent Number
NACA-RM-L6J16a
Report Number: NACA-RM-L6J16a
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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