SURGE AND ROTATING STALL IN AXIAL-FLOW COMPRESSORS .1. THEORETICAL COMPRESSION SYSTEM MODEL

[1] Emmons H. W., 1955, T ASME, V127, P455, DOI DOI 10.1115/1.4014389

[2] GREITZER EM, SURGE ROTATING STA 2

[3] GREITZER EM, 1972, FURTHER INVESTIGATIO

[4] HALFMAN RL, 1962, DYNAMICS, V1, pCH7

[5] HORLOCK JH, 1958, AXIAL FLOW COMPRESSO, pCH7

[6] SOME STALL AND SURGE PHENOMENA IN AXIAL-FLOW COMPRESSORS [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1953, 20 (12): : 835 - 845

[7] HUPPERT MC, 1965, SP36 NASA, pCH12

[8] MARSH H, 1973, 3 I MECH ENGRS C PUB

[9] MCLACHLAN NW, 1956, ORDINARY NONLINEAR D, pCH6

[10] PEARSON CE, 1954, 142 PRATT WHITN RES

[1] Emmons H. W., 1955, T ASME, V127, P455, DOI DOI 10.1115/1.4014389

[2] GREITZER EM, SURGE ROTATING STA 2

[3] GREITZER EM, 1972, FURTHER INVESTIGATIO

[4] HALFMAN RL, 1962, DYNAMICS, V1, pCH7

[5] HORLOCK JH, 1958, AXIAL FLOW COMPRESSO, pCH7

[6] SOME STALL AND SURGE PHENOMENA IN AXIAL-FLOW COMPRESSORS [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1953, 20 (12): : 835 - 845

[7] HUPPERT MC, 1965, SP36 NASA, pCH12

[8] MARSH H, 1973, 3 I MECH ENGRS C PUB

[9] MCLACHLAN NW, 1956, ORDINARY NONLINEAR D, pCH6

[10] PEARSON CE, 1954, 142 PRATT WHITN RES