Prediction of the recirculation zone in supersonic combustor
National conference; 5th, Air breathing engines and aerospace propulsion ; 2000 ; Bangalore, India
01.01.2000
5 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Gas turbine combustor stabilization by heat recirculation
Tema Archiv | 1975
|Gas turbine combustor stabilization by heat recirculation
Kraftfahrwesen | 1975
|