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Modal Interpolation Program, L 215 (INTERP): Supplemental System Design and Maintenance Document - Volume 2The design, structure, and usage of the modal interpolation program L215 are presented. The program uses modal data sets of arrays containing interpolation coefficients. The interpolation arrays are used to determine displacements at various aerodynamic control points. The displacements consist of translations normal to the aerodynamic surface and surface slopes that are parallel and perpendicular to the free stream direction. Five different interpolation methods are available.
Document ID
19790022976
Acquisition Source
Headquarters
Document Type
Contractor Report (CR)
Authors
Hirayama, M. Y. (Boeing Commercial Airplane Co. Seattle, WA, United States)
Kroll, R. I. (Boeing Commercial Airplane Co. Seattle, WA, United States)
Clemmons, R. E. (Boeing Commercial Airplane Co. Seattle, WA, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1979
Publication Information
Publisher: NASA
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-2848
D6-44457
Report Number: NASA-CR-2848
Report Number: D6-44457
Accession Number
79N31147
Funding Number(s)
CONTRACT_GRANT: NAS1-13918
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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