NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Research of the sonic-boom problemWind tunnel tests were conducted to determine the characteristics of sonic booms. A theoretical examination of nonlinear effects in near and far flow fields, as well as sonic boom shock strength, is reported. A study of the Mach lines and bicharacteristics in three dimensional flow was pursued. The direction derivatives if the bicharacteristics were calculated in a general three dimensional flow field. A second order theory for supersonic flow past slender bodies was developed. Formulas relating flow deflections to the Whitham F-function were derived, which permitted determination of the sonic boom strength from wind tunnel measurements fairly close to the body.
Document ID
19740018320
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Drougge, G.
(Aeronautical Research Inst. of Sweden Stockholm., United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1973
Subject Category
Aircraft
Report/Patent Number
NASA-CR-138666
AU-621
Report Number: NASA-CR-138666
Report Number: AU-621
Accession Number
74N26433
Funding Number(s)
CONTRACT_GRANT: NGR-52-120-001
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available