As turbine rotor turns, blades traverse wake zones of nozzle vanes; periodic fluctuation of pressure distribution around circumference of rotor blade is therefore caused; this effect is quantitatively investigated. English translation from Institut fuer Motorenforschung der Luftfahrtforschungsansalt Hermann Goering Mar 1944 n M325/44g.
Pressure distribution measurements on turbine rotor blade passing behind turbine nozzle lattice
Nat Advisory Committee Aeronautics -- Tech Memo
1947
6 pages
Report
Englisch
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