Computation Of Supersonic Flow Over Flying Configurations
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Computation of Supersonic Flow over Flying Configurations
Author | : Adriana Nastase |
Publsiher | : Elsevier |
Total Pages | : 410 |
Release | : 2010-07-07 |
Genre | : Technology & Engineering |
ISBN | : 008055699X |
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Computation of Supersonic Flow over Flying Configurations is a high-level aerospace reference book that will be useful for undergraduate and graduate students of engineering, applied mathematics and physics. The author provides solutions for three-dimensional compressible Navier-Stokes layer subsonic and supersonic flows. Computational work and experimental results show the real-world application of computational results Easy computation and visualization of inviscid and viscous aerodynamic characteristics of flying configurations Includes a fully optimized and integrated design for a proposed supersonic transport aircraft
Supersonic Flow Computations for an ASTOVL Aircraft Configuration
Author | : Sekaripuram Ramakrishnan |
Publsiher | : Unknown |
Total Pages | : 48 |
Release | : 1990 |
Genre | : Aerodynamics, Supersonic |
ISBN | : NASA:31769000513765 |
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Supersonic Flow Computations Over Aerospace Configurations Using an Euler Marching Solver
Author | : Anonim |
Publsiher | : Unknown |
Total Pages | : 124 |
Release | : 1987 |
Genre | : Electronic Book |
ISBN | : NASA:31769000511793 |
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High Angle of Attack Aerodynamics
Author | : Josef Rom |
Publsiher | : Springer Science & Business Media |
Total Pages | : 408 |
Release | : 2012-12-06 |
Genre | : Science |
ISBN | : 9781461228240 |
Download High Angle of Attack Aerodynamics Book in PDF, Epub and Kindle
The aerodynamics of aircraft at high angles of attack is a subject which is being pursued diligently, because the modern agile fighter aircraft and many of the current generation of missiles must perform well at very high incidence, near and beyond stall. However, a comprehensive presentation of the methods and results applicable to the studies of the complex aerodynamics at high angle of attack has not been covered in monographs or textbooks. This book is not the usual textbook in that it goes beyond just presenting the basic theoretical and experimental know-how, since it contains reference material to practical calculation methods and technical and experimental results which can be useful to the practicing aerospace engineers and scientists. It can certainly be used as a text and reference book for graduate courses on subjects related to high angles of attack aerodynamics and for topics related to three-dimensional separation in viscous flow courses. In addition, the book is addressed to the aerodynamicist interested in a comprehensive reference to methods of analysis and computations of high angle of attack flow phenomena and is written for the aerospace scientist and engineer who is familiar with the basic concepts of viscous and inviscid flows and with computational methods used in fluid dynamics.
The Calculation of Downwash Behind Supersonic Wings with an Application to Triangular Plan Forms
Author | : Max A. Heaslet |
Publsiher | : Unknown |
Total Pages | : 726 |
Release | : 1948 |
Genre | : Aerodynamics, Supersonic |
ISBN | : STANFORD:36105024795713 |
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A method is developed, consistent with the assumptions of small perturbation theory, which provides a means of determining for a known load distribution, the downwash behind a wing in supersonic flow. THe analysis is based upon the use of supersonic doublets which are distributed over the plan form and wake of the wing in a manner determined from the wing loading.
Scientific and Technical Aerospace Reports
Author | : Anonim |
Publsiher | : Unknown |
Total Pages | : 456 |
Release | : 1995 |
Genre | : Aeronautics |
ISBN | : UIUC:30112005546491 |
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Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
The Calculation of Three dimensional Supersonic Flows Around Spherically capped Smooth Bodies and Wings Manual for computer programs
Author | : Chong-Wei Chu |
Publsiher | : Unknown |
Total Pages | : 214 |
Release | : 1972 |
Genre | : Aerodynamics, Supersonic |
ISBN | : CORNELL:31924004679027 |
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The Calculation of Three dimensional Supersonic Flows Around Spherically capped Smooth Bodies and Wings Theory and applications
Author | : Chong-Wei Chu |
Publsiher | : Unknown |
Total Pages | : 92 |
Release | : 1972 |
Genre | : Aerodynamics, Supersonic |
ISBN | : CORNELL:31924004679019 |
Download The Calculation of Three dimensional Supersonic Flows Around Spherically capped Smooth Bodies and Wings Theory and applications Book in PDF, Epub and Kindle