High Angle of Attack Aerodynamics

High Angle of Attack Aerodynamics
Author: Josef Rom
Publisher: Springer Science & Business Media
Total Pages: 408
Release: 2012-12-06
Genre: Science
ISBN: 1461228247

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.

Stick & Rudder

Stick & Rudder
Author: Wolfgang Langewiesche
Publisher: McGraw-Hill Companies
Total Pages: 408
Release: 1994
Genre: Science
ISBN:

The classic first analysis of the art of flying is back, now in a special 50th anniversary limited edition with a foreword by Cliff Robertson. leatherette binding, and gold foil stamp. Langewiesche shows precisely what the pilot does when he or she flies, just how it's done, and why.

Glider Flying Handbook

Glider Flying Handbook
Author: Federal Aviation Administration
Publisher: Skyhorse Publishing Inc.
Total Pages: 241
Release: 2007-07
Genre: Education
ISBN: 1602390614

For both certified glider pilots and students attempting certification in the glider category, this is an unparalleled...

Calculation of High Angle of Attack Aerodynamics of Fighter Configurations

Calculation of High Angle of Attack Aerodynamics of Fighter Configurations
Author: Chuan-Tau Edward Lan
Publisher:
Total Pages: 332
Release: 1991
Genre: Angle of attack (Aerodynamics)
ISBN:

A computational method for unsteady aerodynamics of fighter configurations at high angles of attack is developed. The leading-edge vortices are represented by free vortex filaments which are adjusted iteratively to satisfy the force-free condition. The small-disturbance, unsteady potential equation is solved in the frequency domain for motions in pitching, plunging, flapping, side movement, rolling, and yawing oscillation in compressible flow. Computed results in rolling moment coefficients due to side acceleration are compared with data for 60-deg and 80-deg delta wings. Lateral-directional characteristics for an F-106b configuration are also compared with data obtained in forced oscillation tests. It is shown that reasonable results can be obtained by the present unsteady flow method, but not by steady flow theory. Calculation of dynamic stall effects on a rectangular wing of aspect ratio 4 is demonstrated by using experimental section data. Although no data for the wing are available, the results appear plausible. Industrial usage of this has produced mixed results. At this time, the use of these methods in a production manner is recommended.

Flight Vehicle Aerodynamics

Flight Vehicle Aerodynamics
Author: Mark Drela
Publisher: MIT Press
Total Pages: 304
Release: 2014-02-07
Genre: Science
ISBN: 0262526441

An overview of the physics, concepts, theories, and models underlying the discipline of aerodynamics. This book offers a general overview of the physics, concepts, theories, and models underlying the discipline of aerodynamics. A particular focus is the technique of velocity field representation and modeling via source and vorticity fields and via their sheet, filament, or point-singularity idealizations. These models provide an intuitive feel for aerodynamic flow-field behavior and are the basis of aerodynamic force analysis, drag decomposition, flow interference estimation, and other important applications. The models are applied to both low speed and high speed flows. Viscous flows are also covered, with a focus on understanding boundary layer behavior and its influence on aerodynamic flows. The book covers some topics in depth while offering introductions and summaries of others. Computational methods are indispensable for the practicing aerodynamicist, and the book covers several computational methods in detail, with a focus on vortex lattice and panel methods. The goal is to improve understanding of the physical models that underlie such methods. The book also covers the aerodynamic models that describe the forces and moments on maneuvering aircraft, and provides a good introduction to the concepts and methods used in flight dynamics. It also offers an introduction to unsteady flows and to the subject of wind tunnel measurements. The book is based on the MIT graduate-level course “Flight Vehicle Aerodynamics” and has been developed for use not only in conventional classrooms but also in a massive open online course (or MOOC) offered on the pioneering MOOC platform edX. It will also serve as a valuable reference for professionals in the field. The text assumes that the reader is well versed in basic physics and vector calculus, has had some exposure to basic fluid dynamics and aerodynamics, and is somewhat familiar with aerodynamics and aeronautics terminology.

An Introduction to Flapping Wing Aerodynamics

An Introduction to Flapping Wing Aerodynamics
Author: Wei Shyy
Publisher: Cambridge University Press
Total Pages: 321
Release: 2013-08-19
Genre: Science
ISBN: 1107037263

For anyone interested in the aerodynamics, structural dynamics and flight dynamics of small birds, bats, insects and air vehicles (MAVs).

Introduction to Aircraft Flight Mechanics

Introduction to Aircraft Flight Mechanics
Author: Thomas R. Yechout
Publisher: AIAA
Total Pages: 666
Release: 2003
Genre: Aerodynamics
ISBN: 9781600860782

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.