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
Aerodynamic design and analysis system for supersonic aircraft. Part 3: Computer program descriptionThe computer program for the design and analysis of supersonic aircraft configurations is presented. The schematics of the program structure are provided. The individual overlays and subroutines are described. The system is useful in determining surface pressures and supersonic area rule concepts.
Document ID
19750010114
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Middleton, W. D. (Boeing Commercial Airplane Co. Seattle, WA, United States)
Lundry, J. L. (Boeing Commercial Airplane Co. Seattle, WA, United States)
Coleman, R. G. (Boeing Commercial Airplane Co. Seattle, WA, United States)
Date Acquired
September 3, 2013
Publication Date
March 1, 1975
Publication Information
Publisher: NASA
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-2522
D6-41769
Report Number: NASA-CR-2522
Report Number: D6-41769
Accession Number
75N18186
Funding Number(s)
CONTRACT_GRANT: NAS1-12052
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