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Author : Mark R. Nichols
Publisher : Unknown
Page : 128 pages
File Size : 44,5 Mb
Release : 1980
Category : Aerodynamics
ISBN : OCLC:761213621
Author : Anonim
Publisher : Unknown
Page : 102 pages
File Size : 44,9 Mb
Release : 1980
Category : Electronic
ISBN : NASA:31769000549967
Author : Anonim
Publisher : Unknown
Page : 836 pages
File Size : 46,5 Mb
Release : 1994
Category : Aeronautics
ISBN : UIUC:30112067190055
Author : Mark R. Nichols
Publisher : Unknown
Page : 100 pages
File Size : 54,8 Mb
Release : 1980
Category : Aerodynamics
ISBN : UIUC:30112105146044
Author : Anonim
Publisher : Unknown
Page : 492 pages
File Size : 53,7 Mb
Release : 1994
Category : Aeronautics
ISBN : MINN:31951P00691495X
Author : Anonim
Publisher : Unknown
Page : 352 pages
File Size : 43,8 Mb
Release : 1993
Category : Electronic
ISBN : NASA:31769000600653
Author : Anonim
Publisher : Unknown
Page : 170 pages
File Size : 40,5 Mb
Release : 1991
Category : Small business
ISBN : IND:30000068249907
Author : Anonim
Publisher : Unknown
Page : 580 pages
File Size : 48,7 Mb
Release : 1971
Category : Aeronautics
ISBN : STANFORD:36105024715067
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 : Technology Reports Centre (Great Britain)
Publisher : Unknown
Page : 624 pages
File Size : 46,7 Mb
Release : 1981
Category : Electronic
ISBN : STANFORD:36105014644467
Author : Anonim
Publisher : Unknown
Page : 654 pages
File Size : 47,6 Mb
Release : 1992
Category : Aeronautics
ISBN : MINN:31951P00163367D
Author : Anonim
Publisher : Unknown
Page : 1338 pages
File Size : 46,8 Mb
Release : 1981
Category : Science
ISBN : MSU:31293011684952
Author : Anonim
Publisher : Unknown
Page : 942 pages
File Size : 50,7 Mb
Release : 1981
Category : Research
ISBN : UOM:39015034740228
Sections 1-2. Keyword Index.--Section 3. Personal author index.--Section 4. Corporate author index.-- Section 5. Contract/grant number index, NTIS order/report number index 1-E.--Section 6. NTIS order/report number index F-Z.
Author : Wilson Chin
Publisher : John Wiley & Sons
Page : 440 pages
File Size : 44,9 Mb
Release : 2019-04-02
Category : Technology & Engineering
ISBN : 9781119580560
A powerful new monograph from an aerodynamicist reviewing modern conventional aerodynamic approaches, this volume covers aspects of subsonic, transonic and supersonic flow, inverse problems, shear flow analysis, jet engine power addition, engine and airframe integration, and other areas, providing readers with the tools needed to evaluate their own ideas and to implement the newer methods suggested in this book. This new book, by a prolific fluid-dynamicist and mathematician who has published more than twenty research monographs, represents not just another contribution to aerodynamics, but a book that raises serious questions about traditionally accepted approaches and formulations, providing new methods that solve longstanding problems of importance to the industry. While both conventional and newer ideas are discussed, the presentations are readable and geared to advanced undergraduates with exposure to elementary differential equations and introductory aerodynamics principles. Readers are introduced to fundamental algorithms (with Fortran source code) for basic applications, such as subsonic lifting airfoils, transonic supercritical flows utilizing mixed differencing, models for inviscid shear flow aerodynamics, and so on. These are models they can extend to include newer effects developed in the second half of the book. Many of the newer methods have appeared over the years in various journals and are now presented with deeper perspective and integration. This book helps readers approach the literature more critically. Rather than simply understanding an approach, for instance, the powerful "type differencing" behind transonic analysis, or the rationale behind "conservative" formulations, or the use of Euler equation methods for shear flow analysis when they are unnecessary, the author guides and motivates the user to ask why and why not and what if. And often, more powerful methods can be developed using no more than simple mathematical manipulations. For example, Cauchy-Riemann conditions, which are powerful tools in subsonic airfoil theory, can be readily extended to handle compressible flows with shocks, rotational flows, and even three-dimensional wing flowfields, in a variety of applications, to produce powerful formulations that address very difficult problems. This breakthrough volume is certainly a "must have" on every engineer's bookshelf.
Author : Gordon C. Oates
Publisher : AIAA (American Institute of Aeronautics & Astronautics)
Page : 544 pages
File Size : 45,9 Mb
Release : 1989
Category : Science
ISBN : UOM:39015058126494
Annotation The last of three texts on aircraft propulsion technology planned by Gordon C. Oates. Other titles: Aerodynamics of gas turbine and rocket propulsion (1988); Aerothermodynamics of aircraft engine components (1985). Chapters treat combustion technology, engine/airplane performance matching, inlets and inlet/engine integration, variable convergent/divergent nozzle aerodynamics, engine instability, aeroelasticity, and unsteady aerodynamics. Annotation(c) 2003 Book News, Inc., Portland, OR (booknews.com)
Author : Anonim
Publisher : Unknown
Page : 558 pages
File Size : 41,7 Mb
Release : 1984
Category : Aeronautics
ISBN : PSU:000011780670