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Effect of a rectangular simulated wing on the pressure-drag coefficient of various boat tails at Mach numbers from 0.60 to 1.47Wind tunnel tests on conical boattails, nacelles, and rectangular wings
Document ID
19690016947
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Harrington, D. E. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1969
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-52609
Report Number: NASA-TM-X-52609
Accession Number
69N26325
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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