Accession Number : ADA330588
Title : Aerodynamic Flow vectoring of Wakes and Jets for High Lift Control.
Descriptive Note : Final rept. 15 Jun 94-14 Jun 97,
Corporate Author : UNIVERSITY OF SOUTHERN CALIFORNIA LOS ANGELES DEPT OF AEROSPACE ENGINEERING
Personal Author(s) : Redekopp, Larry G.
PDF Url : ADA330588
Report Date : SEP 1997
Pagination or Media Count : 53
Abstract : A methodology has been developed for the aerodynamic flow-vectoring control of wakes on jets. Directional flow control of wakes and jets has been demonstrated without requiring any mechanical motion of the boundaries which constraint or guide the flow. The methodology is based on global instability concepts. The key to the success of this approach is to use local suction to suppress any global instability and then exploit symmetry considerations to produce proportional directional control of this flow.
Descriptors : *JET FIGHTERS, *THRUST VECTOR CONTROL SYSTEMS, INTEGRATED SYSTEMS, TEST METHODS, EDDIES(FLUID MECHANICS), BOUNDARIES, FLOW RATE, WAKE, FLUID DYNAMICS, INSTABILITY, CONTROL JETS.
Subject Categories : Aerodynamics
Attack and Fighter Aircraft
Distribution Statement : APPROVED FOR PUBLIC RELEASE