Aerodynamic Engine/airframe Integration for High Performance Aircraft and Missiles
Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
Publisher:
Published: 1991
Total Pages:
ISBN-13:
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Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
Publisher:
Published: 1991
Total Pages:
ISBN-13:
DOWNLOAD EBOOKAuthor: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
Publisher:
Published: 1992
Total Pages:
ISBN-13: 9789283506720
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Publisher:
Published: 1992
Total Pages: 451
ISBN-13:
DOWNLOAD EBOOKThe 32 papers presented at the AGARD Fluid Dynamics Panel (FDP) symposium on 'Aerodynamic Engine/Airframe Integration for High Performance Aircraft and Missiles' that was held 7th-11th October 1991 in Fort Worth, Texas, United States are contained in this report. In addition to these papers, the Technical Evaluation Report aimed at assessing the relevance and success of the symposium in meeting the technical needs of the aerospace community and the transcript of the Round Table Discussion held at the end of the meeting are included in this document. The objective of the symposium was to review the state-of-art in aerodynamic engine/airframe integration techniques and to report on the progress which has been achieved during engineering project work in recent years. Because the treatment of this subject requires an interdisciplinary approach, both experimentalists and theoreticians were invited to contribute to the meeting. Six sessions were organized to cover the essential sub-disciplines requiring aerodynamic engine/airframe integration during the concept-assessment and design phases for new aerospace vehicles.
Author:
Publisher:
Published: 1994
Total Pages: 956
ISBN-13:
DOWNLOAD EBOOKAuthor: Mark R. Nichols
Publisher:
Published: 1966
Total Pages: 52
ISBN-13:
DOWNLOAD EBOOKAuthor: S. N. B. Murthy
Publisher:
Published: 199?
Total Pages: 570
ISBN-13:
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Publisher:
Published: 1980
Total Pages: 100
ISBN-13:
DOWNLOAD EBOOKAuthor: Wilson C. Chin
Publisher: John Wiley & Sons
Published: 2019-03-21
Total Pages: 349
ISBN-13: 1119580862
DOWNLOAD EBOOKA 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: Mark R. Nichols
Publisher:
Published: 1980
Total Pages: 90
ISBN-13:
DOWNLOAD EBOOKAuthor: S. N. B. Murthy
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
Published: 1986
Total Pages: 568
ISBN-13:
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