Space Transportation System Technology Symposium. Volume 1 - Aerothermodynamics and Configurations
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Page : 582 pages
File Size : 46,89 MB
Release : 1970
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Author :
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Page : 582 pages
File Size : 46,89 MB
Release : 1970
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Page : 772 pages
File Size : 35,86 MB
Release : 1971
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Page : 470 pages
File Size : 19,87 MB
Release : 1972
Category : Aerothermodynamics
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Author : Gloria R. Champine
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Page : 74 pages
File Size : 42,70 MB
Release : 1981
Category : Space shuttles
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Page : 312 pages
File Size : 44,3 MB
Release : 1994
Category : Aeronautics
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Page : 402 pages
File Size : 13,61 MB
Release : 1972
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Author : American Institute of Aeronautics and Astronautics. Ad Hoc Committee on the Assessment of New Space Transportation Systems
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Page : 110 pages
File Size : 29,39 MB
Release : 1973
Category : Launch vehicles (Astronautics)
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Author : John C. Adams (Jr.)
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Page : 240 pages
File Size : 49,77 MB
Release : 1973
Category : Aerodynamics, Hypersonic
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Formulation and application of a windward surface flow-field (inviscid and viscous) analysis is presented for general lifting body configurations at high angles of incidence under hypersonic perfect gas conditions. The technique applies a strip theory concept, leading to an infinite extent yawed body treatment applied in the windward surface crossflow plane for both the inviscid and viscous (boundary layer) flow fields. The boundary-layer analysis is based on the governing equations for yawed blunt body boundary layers.
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Page : 580 pages
File Size : 28,22 MB
Release : 1971
Category : Aeronautics
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A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)
Author : Dieter Jacob
Publisher : John Wiley & Sons
Page : 683 pages
File Size : 19,13 MB
Release : 2006-03-06
Category : Technology & Engineering
ISBN : 3527605509
Focusing on basic aspects of future reusable space transportation systems and covering overall design, aerodynamics, thermodynamics, flight dynamics, propulsion, materials, and structures, this report presents some of the most recent results obtained in these disciplines. The authors are members of three Collaborative Research Centers in Aachen, Munich and Stuttgart concerned with hypersonic vehicles. A major part of the research presented here deals with experimental and numerical aerodynamic topics ranging from low speed to hypersonic flow past the external configuration and through inlet and nozzle. Mathematicians and engineers jointly worked on aspects of flight mechanics like trajectory optimization, stability, control and flying qualities. Structural research and development was predominantly coupled to the needs for high temperature resistant structures for space vehicles.