Performance of annular combustor of turbojet engine was investigated in combustion laboratory to determine whether correlation exists between performance of combustor and altitude operational limits of engine revealed by altitude wind tunnel research. (See also - (discussion) p 278, 344; Nat Advisory Committee Aeronautics -- Tech Note n 1357 July 1947 26 p, 26 supp plates;)
Effect of combustor-inlet conditions on performance of annular turbojet combustor
Soc Automotive Engrs -- Trans
1947
13 pages
Article (Journal)
English
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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
|Effect of COMBUSTOR-INLET CONDITIONS on Combustion in Turbojet Engines
SAE Technical Papers | 1947
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