NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

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

Back to Results
A near-field approach to the sonic boom problemCalculations of shock wave pattern in field surrounding arbitrary aircraft configurations at supersonic speeds based on wing-body analysis methods
Document ID
19680019391
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Woodward, F. A. (Boeing Co. Renton, WA, United States)
Date Acquired
August 4, 2013
Publication Date
August 1, 1967
Subject Category
Aircraft
Report/Patent Number
NASA-CR-73109
D6-15046
Report Number: NASA-CR-73109
Report Number: D6-15046
Accession Number
68N28863
Funding Number(s)
CONTRACT_GRANT: NAS2-3719
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