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Surface pressure data on a series of conical forebodies at Mach numbers from 1.70 to 4.50 and combined angles of attack and sideslipTabulated surface pressure data for a series of forebodies which have analytically defined cross sections and are based on a 20 degs half-angle cone are presented without analysis. Five of the cross sections were ellipses having axis ratios of 3/1, 2/1, 1/1, 1/2, and 1/3. The sixth cross section was defined by a curve having a single lobe. The data generally cover angles of attack from -5 degs to 20 degs at angles of sideslip from 0 degs to 5 degs for Mach numbers of 1.70, 2.50, 3.95, and 4.50 at a constant Reynolds number.
Document ID
19790013879
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Townsend, J. C.
(NASA Langley Research Center Hampton, VA, United States)
Collins, I. K.
(NASA Langley Research Center Hampton, VA, United States)
Howell, D. T.
(NASA Langley Research Center Hampton, VA, United States)
Hayes, C.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
March 1, 1979
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-78808
Accession Number
79N22050
Funding Number(s)
PROJECT: RTOP 505-11-13-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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