Turbojet Engine Diagnostic System based on Compressor Blade Vibration and Vibroacoustic Analysis
Congress; 20th, International Council of Aeronautical Sciences ; 1996 ; Sorrento; Italy
01.01.1996
7 pages
Vol 1 of an unknown no of vols
Aufsatz (Konferenz)
Englisch
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Turbojet Engine Diagnostic System based on Compressor Blade Vibration and Vibroacoustic Analysis
British Library Online Contents | 1996
|Performance of J33-A-27 Turbojet-Engine Compressor
NTRS | 1949
|Performance of J33-A-27 Turbojet-Engine Compressor
NTRS | 1950
|Performance of J33-A-23 Turbojet-Engine Compressor
NTRS | 1948
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