Effect of Liner Air-entry Holes, Fuel State, and Combustor Size on Performance of an Annular Turbojet Combustor at Low Pressures and High Air-flow Rates
13.01.1953
Sonstige
Keine Angabe
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
|