User's Manual for Airfoil Flow Field Computer Code SRAIR
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Page : 64 pages
File Size : 47,48 MB
Release : 1985
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Page : 64 pages
File Size : 47,48 MB
Release : 1985
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Page : 704 pages
File Size : 39,42 MB
Release : 1995
Category : Aeronautics
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Page : 538 pages
File Size : 28,43 MB
Release : 1991
Category : Aeronautics
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Page : 400 pages
File Size : 16,43 MB
Release : 1948
Category : Mechanics, Applied
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Author : Egon Stanewsky
Publisher : Springer Science & Business Media
Page : 432 pages
File Size : 12,89 MB
Release : 2013-04-17
Category : Technology & Engineering
ISBN : 3322907112
This volume contains the description of an EC-sponsered program to study all relevant aspects of shock/ boundary-layer interaction control, the latter designed to improve aircraft performance at design (cruise) and off-design conditions. The work being presented includes a discussion of basic control experiments and the corresponding physical modeling, to account for shock control and a discussion of the airfoil experiments conducted for code validation and control assessment, in conjunction with the basic experiments and computations. The contents is comprised of a section giving a broad overview of the research carried out here and more detailed individual contributions by the participants in the research. Der Band enthält den Abschlußbericht eines von EU geförderten Projekts EUROSHOCK, das alle relevanten Aspekte der Kontrolle von Stoßfronten und Grenzschichten (wichtig z.B. für die Verbesserung der Flugeigenschaften von Fluzeugen) untersuchte. Neben einer ausführlichen Diskussion der grundlegenden Kontrollexperimente und der zugrundeliegenden Modellierung werden auch die Versuche an Tragflächen beschrieben, die zur Validierung von Modellrechnungen durchgeführt werden. Darüber hinaus enthält der Band auch die detaillierten Ergebnisse der Teilnehmer an dem Forschungsprogramm.
Author : Anthony W. Fiore
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Page : 962 pages
File Size : 15,88 MB
Release : 1978
Category : Turbulent boundary layer
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In 1975 the U.S. Air Force and the Federal Republic of Germany signed a Data Exchange Agreement numbered AF-75-G-7440 entitled 'Viscous and Interacting Flow Fields.' The purpose was to exchange data in the area of boundary layer research. It includes both experimental and theoretical boundary layer research at speeds from subsonic to hypersonic Mach numbers in the presence of laminar, transitional, and turbulent boundary layers. The main effort in recent years has been on turbulent boundary layers, both attached and separated in the presence of such parameters as pressure gradients, wall temperature, surface roughness, etc. In the United States the research was conducted in various Department of Defense, NASA, aircraft corporations, and various university laboratories. In the Federal Republic of Germany it was carried out within the various DFVLR, industrial, and university research centers.
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Page : 582 pages
File Size : 44,89 MB
Release : 1985
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Page : 610 pages
File Size : 46,92 MB
Release : 1987
Category : Aeronautics
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Page : 914 pages
File Size : 29,29 MB
Release : 1986
Category : Physics
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Page : 156 pages
File Size : 27,41 MB
Release : 1987
Category : Astronautics
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