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There are a total of 4 record(s) matching your query.
Sorted by: Date Added To NTRS in Descending order
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Design definition study of a NASA/Navy lift/cruise fan technology V/STOL airplane: Risk assessment addendum to the final report
Author(s): Zabinsky, J. M.; Burnham, R. W.; Flora, C. C.; Gotlieb, P.; Grande, D. L.; Gunnarson, D. W.; Howard, W. M.; Hunt, D.; Jakubowski, G. W.; Johnson, P. E., et al.
Abstract: An assessment of risk, in terms of delivery delays, cost overrun, and performance achievement, associated with the V/STOL technology airplane is presented. The risk is discussed in terms of weight, structure, aerodynamics, ...
NASA Center: NASA (non Center Specific) Publication Year: 1975
Added to NTRS: 2008-07-01
Accession Number: 76N18100; Document ID: 19760011012; Report Number: D6-42611-ADD, NASA-CR-137729
Study of metallic structural design concepts for an arrow wing supersonic cruise configuration
Author(s): Turner, M. J.; Grande, D. L.
Abstract: A structural design study was made, to assess the relative merits of various metallic structural concepts and materials for an advanced supersonic aircraft cruising at Mach 2.7. Preliminary studies were made to ensure ...
NASA Center: NASA (non Center Specific) Publication Year: 1977
Added to NTRS: 2005-10-13
Accession Number: 78N16043; Document ID: 19780008100; Report Number: D6-42438-3, NASA-CR-2743
Study of advanced composite structural design concepts for an arrow wing supersonic cruise configuration
Author(s): Turner, M. J.; Grande, D. L.
Abstract: Based on estimated graphite and boron fiber properties, allowable stresses and strains were established for advanced composite materials. Stiffened panel and conventional sandwich panel concepts were designed and analyzed, ...
NASA Center: NASA (non Center Specific) Publication Year: 1978
Added to NTRS: 2005-10-13
Accession Number: 78N20116; Document ID: 19780012173; Report Number: D6-42438-5, NASA-CR-2825
Application of an advanced computerized structural design system to an arrow-wing supersonic cruise aircraft
Author(s): Robinson, J. C.; Yates, E. C., Jr.; Turner, M. J.; Grande, D. L.
Abstract: A structural design study of an arrow-wing supersonic cruise aircraft has been made using the integrated design system, ATLAS, and a relatively large analytical finite-element model containing 8500 degrees of freedom. This ...
NASA Center: Langley Research Center Publication Year: 1975
Added to NTRS: 2004-11-03
Accession Number: 75A39530; Document ID: 19750055458; Report Number: AIAA PAPER 75-1038
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