Volume VII of the High Speed Aerodynamics and Jet Propulsion series. It deals with applications to specific components of the complete aircraft. Sections of the volume include: aerodynamics of wings at high speed, aerodynamics of bodies at high speed, in
[1] Stevens, B. L., and F. L. Lewis,Aircraft Control and Simulation,John Wiley & Sons, New York, 1992 拡張機能 C/C++ コード生成 Simulink® Coder™ を使用して C および C++ コードを生成します。 バージョン履歴 R2006a より前に導入 ...
MILITARY AIRCRAFTSPIN STABILIZATIONAn introduction to, and a broad overiew of, the aerodynamic characteristics of airplanes at high angles of attack are provided. Items include: (1) some important fundamental phenomena which determine the aerodynamic characteristics of airplanes at high angles of attack;...
In conventional force measure wind tunnel test,the balance can get the aerodynamic force of the aircraft and also the directly moment.It is while the press... YM Qin 被引量: 0发表: 2014年 Measurement of pressure center of re-entry vehicle module. In conventional force measure wind tunnel te...
the aerodynamic design results also directly affect the design of the aircraft structure and of the control system. Küchemann [1] presented a comprehensive review of the aerodynamic design of aircraft which included a chapter on the waverider. In fact, the waverider is a special class of the...
Identification of aerodynamic parameters for eccentric bridge section model The equations of motion for bridge deck section model elastically suspended in wind tunnel are formulated about mass center of the system using the Lagrang... Z Chen,H Yan,Y Luo,... - 《Journal of Wind Engineering & ...
The second flight of the Hyper-X program afforded a unique opportunity to determine the aerodynamic force and moment characteristics of an airframe-integrated scramjet-powered aircraft in hypersonic flight. These data were gathered via a repeated series of pitch, yaw, and roll doublets, frequency swe...
The design of electric aircraft is an emerging field, important for decarbonising short-haul passenger transport [1], [2]. Many electric aircraft concepts and prototypes have chosen electric ducted fans (EDFs) for propulsion. In these applications the requirement to operate close to and within ...
In this paper, the authors take the overall configuration of FSW aircraftas their center of attention and discuss the main aerodynamic problems ofoverall configuration--the flow separation at the root part of FSW and theinterference between wing and canard. Starting from the authors' previous ...
Fuller and von Flotow[259]studied active noise control from a commercial standpoint. It was concluded that near-term market penetration of active noise control technology was expected to be through high-tech, expensive applications. The aircraft cabin was proposed as an application field. ...