Performance of experimental channeled-wall annular turbojet combustor at conditions simulating high-altitude supersonic flight I : -U-shaped channel walls for secondary-air entry
15.03.1955
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Englisch
Effect of combustor-inlet conditions on performance of Annular Turbojet Combustor
Engineering Index Backfile | 1947
|Effect of combustor-inlet conditions on performance of annular turbojet combustor
Engineering Index Backfile | 1947
|