Calculated Aerodynamics of Wings in Severe Maneuver
Author : J. E. McCune
Publisher :
Page : 10 pages
File Size : 29,70 MB
Release : 1991
Category : Fluid mechanics
ISBN :
Author : J. E. McCune
Publisher :
Page : 10 pages
File Size : 29,70 MB
Release : 1991
Category : Fluid mechanics
ISBN :
Author :
Publisher :
Page : 568 pages
File Size : 40,22 MB
Release : 1994
Category : Aeronautics
ISBN :
Author : B. M. Cetegen
Publisher :
Page : 12 pages
File Size : 12,79 MB
Release : 1987
Category : Turbulence
ISBN :
Author : W. Z. Stepniewski
Publisher : Courier Corporation
Page : 640 pages
File Size : 20,94 MB
Release : 2013-04-22
Category : Technology & Engineering
ISBN : 0486318516
DIVClear, concise text covers aerodynamic phenomena of the rotor and offers guidelines for helicopter performance evaluation. Originally prepared for NASA. Prefaces. New Indexes. 10 black-and-white photos. 537 figures. /div
Author :
Publisher :
Page : 360 pages
File Size : 17,5 MB
Release : 1993
Category : Aeronautics
ISBN :
Author : Thomas R. Yechout
Publisher : AIAA
Page : 666 pages
File Size : 31,17 MB
Release : 2003
Category : 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.
Author : Wei Shyy
Publisher : Cambridge University Press
Page : 321 pages
File Size : 34,93 MB
Release : 2013-08-19
Category : Science
ISBN : 1107037263
For anyone interested in the aerodynamics, structural dynamics and flight dynamics of small birds, bats, insects and air vehicles (MAVs).
Author :
Publisher :
Page : 2834 pages
File Size : 32,34 MB
Release : 1975
Category : Government publications
ISBN :
Author : Robert C. Nelson
Publisher :
Page : 464 pages
File Size : 29,69 MB
Release : 1998
Category : History
ISBN :
This edition of this this flight stability and controls guide features an unintimidating math level, full coverage of terminology, and expanded discussions of classical to modern control theory and autopilot designs. Extensive examples, problems, and historical notes, make this concise book a vital addition to the engineer's library.
Author : Kirill V. Rozhdestvensky
Publisher : Springer Science & Business Media
Page : 358 pages
File Size : 44,13 MB
Release : 2013-03-09
Category : Technology & Engineering
ISBN : 3662042401
This book is dedicated to the memory of a distinguished Russian engineer, Rostislav E. Alexeyev, who was the first in the world to develop the largest ground effect machine - Ekranoplan. One of Alexeyev's design concepts with the aerodynamic configuration of a jlying wing can be seen on the front page. The book presents a description of a mathematical model of flow past a lifting system, performing steady and unsteady motions in close proximity to the underlying solid surface (ground). This case is interesting for practical purposes because both the aerodynamic and the economic efficiency of the system near the ground are most pronounced. Use of the method of matched asymptotic expansions enables closed form solutions for the aerodynamic characteristics of the wings-in-ground effect. These can be used for design, identification, and processing of experimental data in the course of developing ground effect vehicles. The term extreme ground effect, widely used through out the book, is associated with very small relative ground clearances of the order of 10% or less. The theory of a lifting surface, moving in immediate proximity to the ground, represents one of the few limiting cases that can be treated analytically. The author would like to acknowledge that this work has been influenced by the ideas of Professor Sheila E. Widnall, who was the first to apply the matched asymptotics techniques to treat lifting flows with the ground effect. Saint Petersburg, Russia February 2000 Kirill V. Rozhdestvensky Contents 1. Introduction. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .