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
Calculation of camber using slender wing theory at Mach number 1.0Calculation of mean line camber oridinates for laterally symmetrical wings with polygonal planforms
Document ID
19710024070
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Igoe, W. B. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1971
Subject Category
Aerodynamics
Report/Patent Number
L-7666
NASA-TM-X-2311
Report Number: L-7666
Report Number: NASA-TM-X-2311
Accession Number
71N33546
Funding Number(s)
CONTRACT_GRANT: 136-13-01
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