Author: Massachusetts Institute of TechnologyPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 60
Book Description
Flutter of Low Aspect-ratio Wings: Calculation of pressure distribution for oscillating wings of arbitrary planform in subsonic flow by the kernel-function methods, by Pao-Tan Hsu
Author: Massachusetts Institute of TechnologyPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 60
Book Description
U.S. Government Research Reports
Author: NASA Technical Report
Author: Proceedings (unclassified Portions)
Author: Proceedings of the National Specialists Meeting on Dynamics and Aeroelasticity (unclassified Portions) Fort Worth, Tex., Nov. 6-7, 1958
Author: Institute of the Aerospace SciencesPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 152
Book Description
Bibliography of Scientific and Industrial Reports
Author: Boundary Element Methods in Engineering
Author: Balkrishna S. AnnigeriPublisher: Springer Science & Business Media
ISBN: 3642842380
Category : Technology & Engineering
Languages : en
Pages : 596
Book Description
The Boundary Element Method (BEM) has become established as an effective tool for the solutions of problems in engineering science. The salient features of the BEM have been well documented in the open literature and therefore will not be elaborated here. The BEM research has progressed rapidly, especially in the past decade and continues to evolve worldwide. This Symposium was organized to provide an international forum for presentation of current research in BEM for linear and nonlinear problems in solid and fluid mechanics and related areas. To this end, papers on the following topics were included: rotary wing aerodynamics, unsteady aerodynamics, design and optimization, elasticity, elasto dynamics and elastoplasticity, fracture mechanics, acoustics, diffusion and wave motion, thermal analysis, mathematical aspects and boundary/finite element coupled methods. A special session was devoted to parallel/vector supercomputing with emphasis on mas sive parallelism. This Symposium was sponsored by United Technologies Research Center (UTRC) , NASA Langley Research Center, and the International Association of Boundary Ele ment Methods (lAB EM) . We thank the UTRC management for their permission to host this Symposium. In particular, we thank Dr. Arthur S. Kesten and Mr. Robert E. Olson for their encouragement and support. We gratefully acknowledge the support of Dr. E. Carson Yates, Jr. of NASA Langley, Prof. Luigi Morino, Dr. Thomas A.
Engine Airframe Integration
Author: Consolidated Translation Survey
Author: United States. Central Intelligence Agency. Foreign Documents DivisionPublisher:
ISBN:
Category : Translations
Languages : en
Pages : 208
Book Description
Shock Wave-Boundary-Layer Interactions
Author: Holger BabinskyPublisher: Cambridge University Press
ISBN: 1139498649
Category : Technology & Engineering
Languages : en
Pages : 481
Book Description
Shock wave-boundary-layer interaction (SBLI) is a fundamental phenomenon in gas dynamics that is observed in many practical situations, ranging from transonic aircraft wings to hypersonic vehicles and engines. SBLIs have the potential to pose serious problems in a flowfield; hence they often prove to be a critical - or even design limiting - issue for many aerospace applications. This is the first book devoted solely to a comprehensive, state-of-the-art explanation of this phenomenon. It includes a description of the basic fluid mechanics of SBLIs plus contributions from leading international experts who share their insight into their physics and the impact they have in practical flow situations. This book is for practitioners and graduate students in aerodynamics who wish to familiarize themselves with all aspects of SBLI flows. It is a valuable resource for specialists because it compiles experimental, computational and theoretical knowledge in one place.