AIAA Aircraft Design Systems Meeting: 92-4251
Author :
Publisher :
Page : 382 pages
File Size : 40,65 MB
Release : 1992
Category : Airplanes
ISBN :
Author :
Publisher :
Page : 382 pages
File Size : 40,65 MB
Release : 1992
Category : Airplanes
ISBN :
Author : United States. National Aeronautics and Space Administration
Publisher :
Page : 596 pages
File Size : 41,61 MB
Release :
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ISBN :
Author :
Publisher :
Page : 196 pages
File Size : 49,98 MB
Release : 1990
Category : Industrial engineering
ISBN :
Author :
Publisher :
Page : 472 pages
File Size : 31,53 MB
Release : 1990
Category : Aeronautics
ISBN :
Author : Pasquale M. Sforza
Publisher : Elsevier
Page : 623 pages
File Size : 47,30 MB
Release : 2014-01-31
Category : Technology & Engineering
ISBN : 0124199771
Commercial Airplane Design Principles is a succinct, focused text covering all the information required at the preliminary stage of aircraft design: initial sizing and weight estimation, fuselage design, engine selection, aerodynamic analysis, stability and control, drag estimation, performance analysis, and economic analysis. The text places emphasis on making informed choices from an array of competing options, and developing the confidence to do so. - Shows the use of standard, empirical, and classical methods in support of the design process - Explains the preparation of a professional quality design report - Provides a sample outline of a design report - Can be used in conjunction with Sforza, Manned Spacecraft Design Principles to form a complete course in Aircraft/Spacecraft Design
Author : Jan Roskam
Publisher : DARcorporation
Page : 308 pages
File Size : 12,42 MB
Release : 2002
Category : Biography & Autobiography
ISBN : 9781884885570
Author :
Publisher :
Page : 876 pages
File Size : 29,27 MB
Release : 1995
Category : Airframes
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Page : 416 pages
File Size : 47,46 MB
Release : 1985
Category : Aeronautics
ISBN :
Author : Jiří Čečrdle
Publisher : Elsevier
Page : 378 pages
File Size : 28,32 MB
Release : 2023-01-13
Category : Technology & Engineering
ISBN : 0323955568
Whirl Flutter of Turboprop Aircraft Structures, Second Edition explores the whirl flutter phenomenon, including theoretical, practical, analytical and experimental aspects of the matter. Sections provide a general overview regarding aeroelasticity, discussions on the physical principle and the occurrence of whirl flutter in aerospace practice, and experimental research conducted, especially from the 60s. Other chapters delve into analytical methods such as basic and advanced linear models, non-linear and CFD based methods, certification issues including regulation requirements, a description of possible certification approaches, and several examples of aircraft certification from aerospace. Finally, a database of relevant books, reports and papers is provided. This updated and expanded second edition covers new chapters including both analytical and experimental aspects of the subject matter. - Provides complex information on turboprop aircraft whirl flutter phenomenon - Presents both theoretical and practical (certification related) issues - Includes experimental research as well as analytical models (basic and advanced) of matter - Includes both early-performed works and recent developments - Contains a listing of relevant books and reports
Author : Russell J. Donnelly
Publisher : Springer Science & Business Media
Page : 283 pages
File Size : 18,87 MB
Release : 2012-12-06
Category : Science
ISBN : 1461231086
Liquid helium has been studied for its intrinsic interest through much of the 20th century. In the past decade, much has been learned about heat transfer in liquid helium because of the need to cool superconducting magnets and other devices. The topic of the Seventh Oregon Conference on Low Temperature Physics was an applied one, namely the use of liquid and gaseous helium to generate high Reynolds number flows. The low kinematic viscosity of liquid helium automatically makes high Reynolds numbers accessible and the question addressed in this conference was to explore various possibilities to see what practical devices might be built using liquid or gaseous helium. There are a number of possibilities: construction of a wind tunnel using critical helium gas, free surface testing, low speed flow facilities using helium I and helium ll. At the time of the conference, most consideration had been given to the last possibility because it seemed both possible and useful to build a flow facility which could reach unprecedented Reynolds numbers. Such a device could be useful in pure research for studying turbulence, and in applied research for testing models much as is done in a water tunnel. In order to examine these possibilities in detail, we invited a wide range of experts to Eugene in October 1989 to present papers on their own specialties and to listen to presentations on the liquid helium proposals.