LEADER 01562nam  2200361z- 450 
001 9910346913603321
005 20231214133356.0
010   $a1000016554
035   $a(CKB)4920000000101386
035   $a(oapen)https://directory.doabooks.org/handle/20.500.12854/47768
035   $a(EXLCZ)994920000000101386
100   $a20202102d2010      |y             0
101 0 $aeng
135   $aurmn|---annan
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aFlow control : theoretical concept of absolute instability
210   $cKIT Scientific Publishing$d2010
215   $a1 electronic resource (97 p. p.)
311   $a3-86644-531-8 
330   $aAt the 37th Prandtl memorial lecture on Regions of Viccous Flow, H.Oertel 1994 developed for the first time the stability theory of local perturbations in boundary layers and wake flows, as well as their practical application in the flow control of vehicle flows and the boundary layer of civil aircraft wings.This work presents how the stability theory concept of absolute instability has advanced and proven in practice in the last 15 years in terms of the efficient flow control.
517   $aFlow control 
610   $aFlow Control
610   $aFluid Mechanics
610   $aStability Theory
610   $aWake Flow
610   $aBundary Layer Transition
700   $aOertel$b Herbert$4auth$02642
906   $aBOOK
912   $a9910346913603321
996   $aFlow control : theoretical concept of absolute instability$93038093
997   $aUNINA