International Aerospace Abstracts
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Page : 1016 pages
File Size : 21,33 MB
Release : 1999
Category : Aeronautics
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Author :
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Page : 1016 pages
File Size : 21,33 MB
Release : 1999
Category : Aeronautics
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Author :
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Page : 704 pages
File Size : 14,90 MB
Release : 1995
Category : Aeronautics
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Author : American Institute of Aeronautics and Astronautics
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Page : 868 pages
File Size : 36,90 MB
Release : 2005
Category : Aeronautics
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Author :
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Page : 1150 pages
File Size : 49,17 MB
Release : 1996
Category : Aeronautics
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Page : 712 pages
File Size : 32,92 MB
Release : 1993
Category : Aeronautics
ISBN :
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)
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Page : 654 pages
File Size : 26,6 MB
Release : 1992
Category : Aeronautics
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Page : 1334 pages
File Size : 19,30 MB
Release : 1991
Category : Government reports announcements & index
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Page : 422 pages
File Size : 28,28 MB
Release : 2001
Category : Mechanics, Applied
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Author : American Institute of Aeronautics and Astronautics. Technical Information Service
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Page : 184 pages
File Size : 17,89 MB
Release : 1996
Category : AIAA paper
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Author : Mårten T. Landahl
Publisher : Courier Dover Publications
Page : 147 pages
File Size : 28,91 MB
Release : 2019-04-17
Category : Science
ISBN : 0486832775
This classic monograph on unsteady transonic flow — the flow of air encountered at speeds at or near the speed of sound — is of continuing interest to students and professionals in aerodynamics, fluid dynamics, and other areas of applied mathematics. After a brief Introduction, Swedish physicist Mårten T. Landahl presents a chapter in which the two-dimensional solution is derived, succeeded by a discussion of its relation to the subsonic and supersonic solutions. Three chapters on low aspect ratio configurations follow, covering triangular wings and similar planforms with curved leading edges, rectangular wings, and cropped delta wings, and low aspect ratio wing-body combinations. The treatment concludes with a consideration of the experimental determination of air forces on oscillating wings at transonic speeds.