Author: Publisher:
ISBN:
Category : Science
Languages : en
Pages : 166
Book Description
NASA Technical Paper
Author: Aerodynamic Characteristics at Mach Numbers from to 1.6 to 2.8 of 74 Deg. Swept Arrow Wings with and Without Camber and Twist
Author: Survey and Analysis of Research on Supersonic Drag-due-to-lift Minimization with Recommendations for Wing Design
Author: Harry W. CarlsonPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 164
Book Description
Scientific and Technical Aerospace Reports
Author: AIAA 78-78 - AIAA 78-139
Author: A Higher Order Panel Method for Linearized Supersonic Flow
Author: F. Edward EhlersPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 260
Book Description
Proceedings of the ... Congress of the International Council of the Aeronautical Sciences
Author: International Council of the Aeronautical Sciences. CongressPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 748
Book Description
Aeronautical Engineering
Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 716
Book Description
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).
Introduction to Aircraft Flight Mechanics
Author: Thomas R. YechoutPublisher: AIAA
ISBN: 9781600860782
Category : Aerodynamics
Languages : en
Pages : 666
Book Description
Based on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.
High Angle of Attack Aerodynamics
Author: Josef RomPublisher: Springer Science & Business Media
ISBN: 1461228247
Category : Science
Languages : en
Pages : 408
Book Description
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.