COMPARISON OF MEASURED AND PREDICTED FLOWS THROUGH CONICAL SUPERSONIC NOZZLES WITH EMPHASIS ON TRANSONIC REGION

[1] TRUNCATED PERFECT NOZZLES IN OPTIMUM NOZZLE DESIGN [J]. ARS JOURNAL, 1961, 31 (05): : 614 - 620

[2] SHOCK-INDUCED BOUNDARY LAYER SEPARATION IN OVEREXPANDED CONICAL EXHAUST NOZZLES [J]. AIAA JOURNAL, 1963, 1 (03) : 578 - 581

[3] ARENS M, 1962, B RES COUNCIL ISRAEL, VC 11, P45

[4] Back L.H., 1964, INT J HEAT MASS TRAN, V7, P549, DOI [10.1016/0017-9310(64)90052-3, DOI 10.1016/0017-9310(64)90052-3]

[5] CAMPBELL CE, 1960, NASATND467

[6] DARWELL HM, 1963, AIAA J, V1, P1932

[7] ELLIOTT DG, 1963, TR32387 JET PROP LAB

[8] FORTINI A, 1963, NASATND1743

[9] FRAZER RP, 1959, J MECH ENG SCI, V1, P267

[10] HALL IM, 1962, Q J MECH APPL MATH, V15, P487, DOI 10.1093/qjmam/15.4.487

[1] TRUNCATED PERFECT NOZZLES IN OPTIMUM NOZZLE DESIGN [J]. ARS JOURNAL, 1961, 31 (05): : 614 - 620

[2] SHOCK-INDUCED BOUNDARY LAYER SEPARATION IN OVEREXPANDED CONICAL EXHAUST NOZZLES [J]. AIAA JOURNAL, 1963, 1 (03) : 578 - 581

[3] ARENS M, 1962, B RES COUNCIL ISRAEL, VC 11, P45

[4] Back L.H., 1964, INT J HEAT MASS TRAN, V7, P549, DOI [10.1016/0017-9310(64)90052-3, DOI 10.1016/0017-9310(64)90052-3]

[5] CAMPBELL CE, 1960, NASATND467

[6] DARWELL HM, 1963, AIAA J, V1, P1932

[7] ELLIOTT DG, 1963, TR32387 JET PROP LAB

[8] FORTINI A, 1963, NASATND1743

[9] FRAZER RP, 1959, J MECH ENG SCI, V1, P267

[10] HALL IM, 1962, Q J MECH APPL MATH, V15, P487, DOI 10.1093/qjmam/15.4.487