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A finite-step method for calculation of theoretical load distributions for arbitrary lifting surface arrangements at subsonic speedsLoad distribution calculations for subsonic compressible flow of arbitrary wings and lifting surfaces
Document ID
19690021959
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Blackwell, J. A., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1969
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-5335
Report Number: NASA-TN-D-5335
Accession Number
69N31337
Funding Number(s)
CONTRACT_GRANT: 126-13-01-29-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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