Proceedings for the nineteenth annual techfest are accompanied by visual displays for selected topics. Selected topics in structures include limit-cycle oscillations of aircraft lifting surfaces; automated airframe monitoring; low-cost, high-performance target drone wing manufacturing process comparison; and elevated temperature testing considerations for various material systems. Experimental methods and instrumentation that were discussed included low-cost piloted flight simulation, and overview of doppler global velocimetry, and overview of the NIAR crash-dynamics lab, modernization of the Walter Beech Wind Tunnel, development of a PC-based real-time PCM display and analysis system. Topics in aerodynamics include axial flow fan research underway at the University of Kansas, axial agility and pitch agility of fighter aircraft revisited, an experimental and numerical investigation of a 70 degree delta wing at high angles of attack, and the adaptation of ACSYNT for business jet configuration synthesis.
Aiaa Techfest 29 Proceedings
1993
217 pages
Report
Keine Angabe
Englisch
Aerodynamics , Aeronautics , Aircraft , Aerodynamic stability , Aircraft configurations , Airfoil oscillations , Airframes , Axial flow , Flight control , Flight simulation , Target drone aircraft , Control surfaces , Delta wings , Fighter aircraft , Low cost , Manufacturing , Turbofans , Velocity measurement , Wind tunnels , Meetings
NTIS | 1994
|Online Contents | 2007
Online Contents | 1997