-
1
-
-
85007699736
-
Study of the highly underexpanded sonic jet
-
Crist,S., Sherman,P.M., Glass,D.R., Study of the Highly Underexpanded Sonic Jet, AIAA J.Vol.4,No.1, (1966),68-71.
-
(1966)
AIAA J.
, vol.4
, Issue.1
, pp. 68-71
-
-
Crist, S.1
Sherman, P.M.2
Glass, D.R.3
-
3
-
-
85007661609
-
Mach disk in underexpanded exhaust plumes
-
Abbett,M., Mach Disk in Underexpanded Exhaust Plumes,AIAA J.Vol.9,No.3,(1971),pp.512-514.
-
(1971)
AIAA J.
, vol.9
, Issue.3
, pp. 512-514
-
-
Abbett, M.1
-
4
-
-
85003290958
-
A correlation of freejet data
-
Drifmyer,R.T., A Correlation of Freejet Data, AIAA J.Vol.10,No.8, (1972), pp.1093-1095.
-
(1972)
AIAA J.
, vol.10
, Issue.8
, pp. 1093-1095
-
-
Drifmyer, R.T.1
-
5
-
-
0019354196
-
Effects of axisymmetric sonic nozzle geometry on Mach disk characteristics
-
Addy,A.L.,Effects of Axisymmetric Sonic Nozzle Geometry on Mach Disk Characteristics, AIAA J.,19,No1, (1981), pp.121-122.
-
(1981)
AIAA J.
, vol.19
, Issue.1
, pp. 121-122
-
-
Addy, A.L.1
-
6
-
-
0002878296
-
On the structure of jets from highly underexpanded nozzles into still air
-
Adamson, Jr.T.C., Nicholls,J.A.,On the Structure of Jets from Highly Underexpanded Nozzles into Still Air,J.Aero/Space Sci.Vol.26, (1959), pp.16-24.
-
(1959)
J. Aero/Space Sci.
, vol.26
, pp. 16-24
-
-
Adamson Jr., T.C.1
Nicholls, J.A.2
-
7
-
-
85003368843
-
Location of the normal shock wave in the exhaust plume of a jet
-
Eastman,D.W., Radtke,L.P., Location of the Normal Shock Wave in the Exhaust Plume of a Jet, AIAA J.Vol.1,No.4, (1963), pp.918-919.
-
(1963)
AIAA J.
, vol.1
, Issue.4
, pp. 918-919
-
-
Eastman, D.W.1
Radtke, L.P.2
-
8
-
-
0015971564
-
On the structure of jet plumes
-
Fox,J., On the Structure of jet Plumes, AIAA J.Vol.12,No.1, (1974), pp.105-107.
-
(1974)
AIAA J.
, vol.12
, Issue.1
, pp. 105-107
-
-
Fox, J.1
-
9
-
-
0016091424
-
Mach disk from underexpanded axisymmetric nozzle flow
-
Chang,I.S., Chow,W.L., Mach Disk from Underexpanded Axisymmetric Nozzle Flow, AIAA J.Vol.12,No.8,(1974),pp.1079-1082.
-
(1974)
AIAA J.
, vol.12
, Issue.8
, pp. 1079-1082
-
-
Chang, I.S.1
Chow, W.L.2
-
10
-
-
0022667889
-
Numerical simulation and visualization of freejet flow-fields
-
Saito,T., Nakatsuji,H., Teshima,K., Numerical Simulation and Visualization of Freejet Flow-Fields, Trans.Japan Soc.Aero.Space Sci.,Vol.28,No.82,(1986), pp.240-247.
-
(1986)
Trans. Japan Soc. Aero. Space Sci.
, vol.28
, Issue.82
, pp. 240-247
-
-
Saito, T.1
Nakatsuji, H.2
Teshima, K.3
-
11
-
-
0344123602
-
Numerical and experimental studies on choked underexpanded jets
-
Matsuda,T, Umeda,Y., Ishii,R., Yasuda,A., Numerical and Experimental Studies on Choked Underexpanded Jets, AIAA Paper87-1378,(1987), pp.1-11.
-
(1987)
AIAA Paper
, vol.87
, Issue.1378
, pp. 1-11
-
-
Matsuda, T.1
Umeda, Y.2
Ishii, R.3
Yasuda, A.4
-
12
-
-
0006615499
-
Application of method of characteristics to underezpanded, freejet flows with vibrational nonequilibrium
-
Jennifer,L.P., Ronald,K.H., Application of Method of Characteristics to Underezpanded, Freejet Flows with Vibrational Nonequilibrium, AIAA J.Vol.36,No.2,(1998), pp.193-200.
-
(1998)
AIAA J.
, vol.36
, Issue.2
, pp. 193-200
-
-
Jennifer, L.P.1
Ronald, K.H.2
-
13
-
-
0034419822
-
Pitit pressures of correctly-expanded and underexpanded free jets from axisymmetric supersonic nozzles
-
Katanoda,H., Miyazato,Y., Masuda,M., Matsuo,K., Pitit Pressures of Correctly-Expanded and Underexpanded Free Jets from Axisymmetric Supersonic Nozzles,Shock Waves, vol.10, No.2, (2000), pp.95-101.
-
(2000)
Shock Waves
, vol.10
, Issue.2
, pp. 95-101
-
-
Katanoda, H.1
Miyazato, Y.2
Masuda, M.3
Matsuo, K.4
-
14
-
-
0036948436
-
Scaling parameters for underexpanded supersonic jets
-
Yüceil,K.B., Ötügen,M.V., Scaling parameters for underexpanded supersonic jets,Phys. Fluids,Vol.14, No.12,(2002), pp.4206-4215.
-
(2002)
Phys. Fluids
, vol.14
, Issue.12
, pp. 4206-4215
-
-
Yüceil, K.B.1
Ötügen, M.V.2
-
15
-
-
21844509676
-
Numerical confirmation of the hysteresis phenomenon in the regular to the Mach reflection transition in the steady flows
-
Chpoun, A.,Ben-Dor,G., Numerical confirmation of the hysteresis phenomenon in the regular to the Mach reflection transition in the steady flows, Shock Waves, 5,4, (1995), pp. 199-203.
-
(1995)
Shock Waves
, vol.5
, Issue.4
, pp. 199-203
-
-
Chpoun, A.1
Ben-Dor, G.2
-
16
-
-
0029347415
-
Reconsideration of the state-of-the-art of the shock wave reflection phenomenon in steady flows
-
Ben-Dor,G., Reconsideration of the State-of-the-Art of the Shock Wave Reflection Phenomenon in Steady Flows, Jap. Soc. of Mech. Eng. Int. J, B,38,3,(1995), pp.325-334.
-
(1995)
Jap. Soc. of Mech. Eng. Int. J, B
, vol.38
, Issue.3
, pp. 325-334
-
-
Ben-Dor, G.1
-
17
-
-
0035339344
-
Flow-Mach-number-variation-induced hysteresis in steady shock wave reflections
-
Ivanov, M.S. et al., Flow-Mach-Number-Variation-Induced Hysteresis in Steady Shock Wave Reflections, AIAA J., Vol.39,No.5, (2001), pp.972-974.
-
(2001)
AIAA J.
, vol.39
, Issue.5
, pp. 972-974
-
-
Ivanov, M.S.1
-
18
-
-
0035641245
-
Transition between regular and Mach reflection of shock waves: New numerical and experimental results
-
Ivanov, M.S. et al., Transition between regular and Mach reflection of shock waves: new numerical and experimental results, Shock Waves, 11,3,199-207(2001).
-
(2001)
Shock Waves
, vol.11
, Issue.3
, pp. 199-207
-
-
Ivanov, M.S.1
-
19
-
-
0035842119
-
Hysteresis phenomena in the interaction process of conical shock waves: Experimental and numerical investigations
-
BEN-DOR, G. et al., Hysteresis phenomena in the interaction process of conical shock waves: experimental and numerical investigations, J. Fluid Mech. Vol.448, (2001), pp.147-174.
-
(2001)
J. Fluid Mech.
, vol.448
, pp. 147-174
-
-
Ben-Dor, G.1
-
20
-
-
0036588568
-
Hysteresis processes in the regular reflection ↔Mach reflection transition in steady flows
-
BEN-DOR, G. et al., Hysteresis processes in the regular reflection ↔Mach reflection transition in steady flows, progress in Aero. Sci. 38,(2002), pp.347-387.
-
(2002)
Progress in Aero. Sci.
, vol.38
, pp. 347-387
-
-
Ben-Dor, G.1
-
21
-
-
21244451700
-
Shock structure of a supersonic free jet issuing from a rectangular orifice
-
Japan'92, (in Japanese)
-
Teshima, K., Shock Structure of a Supersonic Free Jet Issuing from a Rectangular Orifice, Proc. of Symp. on Shock Waves, Japan'92, (1993),pp. 473-476.(in Japanese).
-
(1993)
Proc. of Symp. on Shock Waves
, pp. 473-476
-
-
Teshima, K.1
-
22
-
-
0034140218
-
Numerical study of shock-reflection hysteresis in an underexpanded jet
-
Gribben, B.J. et al., Numerical Study of Shock-Reflection Hysteresis in an Underexpanded Jet, AIAA J., Vol.38,No.2, (2000), pp.275-283.
-
(2000)
AIAA J.
, vol.38
, Issue.2
, pp. 275-283
-
-
Gribben, B.J.1
-
23
-
-
0003264183
-
Upwind and symmetric shock-capturing schemes
-
Yee, H. C., Upwind and symmetric shock-capturing schemes, NASA TM 89464, (1987), pp. 1-127.
-
(1987)
NASA TM 89464
, pp. 1-127
-
-
Yee, H.C.1
-
24
-
-
0017632872
-
A numerical study of a converging cylindrical shock
-
Sod, G. A., A numerical study of a converging cylindrical shock, J. Fluid Mech., Vol.83, Part 4, (1977), pp.785-794.
-
(1977)
J. Fluid Mech.
, vol.83
, Issue.4 PART
, pp. 785-794
-
-
Sod, G.A.1
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