Subsonic Transonic Configuration Aerodynamics
DOWNLOAD
Download Subsonic Transonic Configuration Aerodynamics PDF/ePub or read online books in Mobi eBooks. Click Download or Read Online button to get Subsonic Transonic Configuration Aerodynamics book now. This website allows unlimited access to, at the time of writing, more than 1.5 million titles, including hundreds of thousands of titles in various foreign languages. If the content not found or just blank you must refresh this page
Subsonic Transonic Configuration Aerodynamics
DOWNLOAD
Author : ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT NEUILLY-SUR-SEINE (France)
language : en
Publisher:
Release Date : 1980
Subsonic Transonic Configuration Aerodynamics written by ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT NEUILLY-SUR-SEINE (France) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1980 with categories.
An important region of the flight envelope of military aircraft is the transonic regime where fighter aircraft must undergo agile maneuvers, and airlift aircraft must cruise efficiently. Unfortunately it is a speed regime where wind tunnel testing is difficult, and numerical computations are not yet fully viable. Most troublesome is that exact configuration optimization criteria are lacking. Unavoidably the optimization procedure has been an ad hoc procedure, depending on the intuitive skills of the aerodynamicist. During the past decade, there has been significant progress in the development of transonic wind tunnel test techniques and computational methods. Employing these techniques, the aerodynamicist has developed many imaginative design concepts that have added to the optimization data base. It was the purpose of the symposium to review and assess these developments and project the future. Twenty nine papers comprised the meeting with three invited review papers. There was a relatively even mixture of theoretical and experimental papers with many providing test/theory comparisons. Subject matter ranged from simple wing-fuselage interference for both fighter and airlift configurations to those envolving additional components such as nacelle and pylons, powered jets, winglets, and most importantly stores and weapons.
Technical Evaluation Report On The Fluid Dynamics Panel Symposium On Subsonic Transonic Configuration Aerodynamics
DOWNLOAD
Author : Horst Körner
language : en
Publisher:
Release Date : 1981
Technical Evaluation Report On The Fluid Dynamics Panel Symposium On Subsonic Transonic Configuration Aerodynamics written by Horst Körner and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1981 with Aerodynamics categories.
The AGARD Fluid Dynamics Panel held its spring symposium 1980 on Subsonic/Transonic Configuration Aerodynamics at the Hochschule der Bundeswehr Munchen, Neubiberg, 5-7 May, 1980. The requirement of improved performance of military combat and airlift aircraft requires not only highly refined point designs at specific flight conditions, but also mission design to maintain optimal performance over the flight spectrum; for instance, by variable geometry concepts. Of particular importance here is the aerodynamic design of the wing, fuselage, components of the empennage, external and conformal stores, fuselage and wing-mounted nacelle-pylons with their powered jet exhausts at subsonic and transonic Mach numbers such that each component achieves optimal performance under the influence of the other components. Here, not only must adverse interference effects be eliminated, but positive favorable interference must be sought. There have been great strides recently in the understanding of aerodynamic interference through more carefully conducted and highly diagnosed windtunnel tests, as well as by the availability of versatile computer codes and powerful computers. It will be the aim of the Symposium to report on these accomplishments. Vectored thrust in the context with V/STOL in excluded. With this scope the meeting was a direct successor of the FDP-Symposium Aerodynamic Interference held in autumn 1970. At that time the solution of aerodynamic interference problems at subsonic and supersonic speed became feasible with the development of panel methods.
High Angle Of Attack Aerodynamics
DOWNLOAD
Author : Josef Rom
language : en
Publisher: Springer Science & Business Media
Release Date : 2012-12-06
High Angle Of Attack Aerodynamics written by Josef Rom and has been published by Springer Science & Business Media this book supported file pdf, txt, epub, kindle and other format this book has been release on 2012-12-06 with Science categories.
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.
Special Course On Subsonic Transonic Aerodynamic Interference For Aircraft
DOWNLOAD
Author : ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT NEUILLY-SUR-SEINE (France)
language : en
Publisher:
Release Date : 1983
Special Course On Subsonic Transonic Aerodynamic Interference For Aircraft written by ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT NEUILLY-SUR-SEINE (France) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1983 with categories.
This course was a follow-up to an AGARD Fluid Dynamics Panel Symposium on Subsonic/Transonic Configuration Aerodynamics. The emphasis of the course was on the configuration optimization in the transonic regime where both military and commercial aircraft must cruise efficiently and where military aircraft must maneuver in an agile but stable manner. The course material was updated and presented in a more structured fashion emphasizing the fluid dynamic interference mechanisms that are the keys to the optimization. In addition, some aspects of subcritical interference were also covered, including those arising in the takeoff and landing phase of the flight with high lift devices deployed. Specific topics include: Subsonic/Transonic Aerodynamic Interference for Aircraft; Computational Methods for Subsonic and Transonic Aerodynamic Design; Subsonic/Transonic Viscous Interactions; Transonic Airfoil Development; Application of Computational Procedures in Aerodynamic Design; Transonic Empirical Configuration Design Process; External Stores Interference; and Engine/Airframe Interference.
Subsonic Transonic Configuration Aerodynamics
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1980
Subsonic Transonic Configuration Aerodynamics written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1980 with Aerodynamics categories.
Subsonic Aerodynamic Characteristics Of The Hl 20 Lifting Body Configuration
DOWNLOAD
Author : George M. Ware
language : en
Publisher:
Release Date : 1993
Subsonic Aerodynamic Characteristics Of The Hl 20 Lifting Body Configuration written by George M. Ware and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1993 with Aerodynamics categories.
Subsonic Transonic And Supersonic Aerodynamic Characteristics Of A Modified Arrow Wing Transport Airplane Configuration
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1964
Subsonic Transonic And Supersonic Aerodynamic Characteristics Of A Modified Arrow Wing Transport Airplane Configuration written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1964 with categories.
Technical Evaluation Report On The Fluid Dynamics Panel Symposium On Subsonic Transonic Configuration Aerodynamics
DOWNLOAD
Author : Dr-Ing Horst Korner
language : en
Publisher:
Release Date : 1979
Technical Evaluation Report On The Fluid Dynamics Panel Symposium On Subsonic Transonic Configuration Aerodynamics written by Dr-Ing Horst Korner and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1979 with categories.
Subsonic Aerodynamic Characteristics Of An Airplane Configuration Utilizing A Variable Sweep Wing Having A Free Floating Apex
DOWNLOAD
Author : Edward Charles Polhamus
language : en
Publisher:
Release Date : 1965
Subsonic Aerodynamic Characteristics Of An Airplane Configuration Utilizing A Variable Sweep Wing Having A Free Floating Apex written by Edward Charles Polhamus and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with Aerodynamics categories.
Wind Tunnel Studies At Subsonic And Transonic Speeds Of A Multiple Mission Variable Wing Sweep Airplane Configuration
DOWNLOAD
Author : William J. Alford
language : en
Publisher:
Release Date : 1959
Wind Tunnel Studies At Subsonic And Transonic Speeds Of A Multiple Mission Variable Wing Sweep Airplane Configuration written by William J. Alford and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with Aerodynamics categories.