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 Soc Automotive Engrs -- Trans v 1 n 2 Apr 1947 p 266-78 (discussion) 278, 344)
Effect of combustor-inlet conditions on performance of annular turbojet combustor
Nat Advisory Committee Aeronautics -- Tech Note
1947
26 pages
26 Supp Plates
Article (Journal)
English
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Effect of combustor-inlet conditions on performance of Annular Turbojet Combustor
Engineering Index Backfile | 1947
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