NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
A non-axisymmetric linearized supersonic wave drag analysis: Mathematical theoryA Mathematical theory is developed to perform the calculations necessary to determine the wave drag for slender bodies of non-circular cross section. The derivations presented in this report are based on extensions to supersonic linearized small perturbation theory. A numerical scheme is presented utilizing Fourier decomposition to compute the pressure coefficient on and about a slender body of arbitrary cross section.
Document ID
19960027894
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Barnhart, Paul J. (NYMA, Inc. Brook Park, OH United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1996
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.26:198430
NASA-CR-198430
E-10030
Report Number: NAS 1.26:198430
Report Number: NASA-CR-198430
Report Number: E-10030
Accession Number
96N29036
Funding Number(s)
PROJECT: RTOP 505-60-00
CONTRACT_GRANT: NAS3-27186
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available