-
1
-
-
0001254490
-
On the noise emanating from a two-dimensional jet above the critical pressure
-
A. POWELL 1953 Aeronautical Quarterly 4, 103-122. On the noise emanating from a two-dimensional jet above the critical pressure.
-
(1953)
Aeronautical Quarterly
, vol.4
, pp. 103-122
-
-
Powell, A.1
-
3
-
-
0001376961
-
On edgetones and associated phenomena
-
A. POWELL 1953 Acustica 3, 233-243. On edgetones and associated phenomena.
-
(1953)
Acustica
, vol.3
, pp. 233-243
-
-
Powell, A.1
-
5
-
-
0040707511
-
The near noise field of static jets and some model studies of devices for noise reduction
-
L. W. LASSITER and H. H. HUBBARD 1954 NACA TN 3187. The near noise field of static jets and some model studies of devices for noise reduction.
-
(1954)
NACA TN
, pp. 3187
-
-
Lassiter, L.W.1
Hubbard, H.H.2
-
6
-
-
0038929560
-
Sur la fre'quencies des sondes e'mises par un jet d'air 'a grand vitesse
-
M. MERLE 1956 C. R. Academy of Science Paris 243, 490-493. Sur la fre'quencies des sondes e'mises par un jet d'air 'a grand vitesse.
-
(1956)
C. R. Academy of Science Paris
, vol.243
, pp. 490-493
-
-
Merle, M.1
-
7
-
-
0039134881
-
Tones from a choked axisymmetric jet. I. Cell structure, eddy velocity and source locations
-
M. G. DAVIES and D. E. S. OLDFIELD 1962 Acustica 12, 257-266. Tones from a choked axisymmetric jet. I. cell structure, eddy velocity and source locations.
-
(1962)
Acustica
, vol.12
, pp. 257-266
-
-
Davies, M.G.1
Oldfield, D.E.S.2
-
8
-
-
0039134881
-
Tones from a choked axisymmetric jet. II. The self excited loop and mode of oscillation
-
M. G. DAVIES and D. E. S. OLDFIELD 1962 Acustica 12, 267-277. Tones from a choked axisymmetric jet. II. the self excited loop and mode of oscillation.
-
(1962)
Acustica
, vol.12
, pp. 267-277
-
-
Davies, M.G.1
Oldfield, D.E.S.2
-
10
-
-
0040707514
-
On the production of discrete frequencies in the noise spectrum of a supersonic jet
-
L. J. POLDERVAART, A. P. WIJNANDS and F. H. M. JONGSMA 1968 Meeting of the Noise Research Committee of the Aeronautical Research Council held at the Royal Aeronautical Society, 4, Hamilton Place, London (also T. H. Eindhoven Report). On the production of discrete frequencies in the noise spectrum of a supersonic jet.
-
(1968)
Meeting of the Noise Research Committee of the Aeronautical Research Council Held at the Royal Aeronautical Society, 4, Hamilton Place, London (Also T. H. Eindhoven Report)
, vol.4
-
-
Poldervaart, L.J.1
Wijnands, A.P.2
Jongsma, F.H.M.3
-
11
-
-
0038929559
-
Aerosonic games with the aid of control elements and externally generated pulses
-
L. J. POLDERVAART, A. P. J. WIJNANDS and L. BRONKHURST 1973 AGARD CP-131, 1-4. Aerosonic games with the aid of control elements and externally generated pulses.
-
(1973)
AGARD
, vol.CP-131
, pp. 1-4
-
-
Poldervaart, L.J.1
Wijnands, A.P.J.2
Bronkhurst, L.3
-
13
-
-
0008081178
-
An investigation of the near noise fields of a choked axisymmetric jet
-
H. B. RIBNER, editor. Toronto: University of Toronto Press. Proceedings of AFOSR-V. T. A. S. Symposium held at Toronto, 20-21 May
-
R. WESTLEY and J. H. WOOLLEY 1968 Aerodynamic Noise (H. B. RIBNER, editor). Toronto: University of Toronto Press. Proceedings of AFOSR-V. T. A. S. Symposium held at Toronto, 20-21 May, 147-167. An investigation of the near noise fields of a choked axisymmetric jet.
-
(1968)
Aerodynamic Noise
, pp. 147-167
-
-
Westley, R.1
Woolley, J.H.2
-
15
-
-
84907164006
-
Flow and sound visualization of an axisymmetric choked jet (10 in schlieren). (16 mm, silent film, running time 8-5 min)
-
R. WESTLEY and J. H. WOOLLEY 1968 National Research Council of Canada, National Aeronautical Establishment YC. NRC, ME. Film No. 13, June 1968. Flow and sound visualization of an axisymmetric choked jet (10 in schlieren). (16 mm, silent film, running time 8-5 min).
-
(1968)
National Research Council of Canada, National Aeronautical Establishment YC. NRC, ME. Film No. 13, June 1968
, vol.13
-
-
Westley, R.1
Woolley, J.H.2
-
17
-
-
85030066358
-
Flow and sound visualization of an axisymmetric choked jet (24 in schlieren). (16 mm, silent film, running time 10 min)
-
R. WESTLEY and J. H. WOOLLEY 1969 National Research Council of Canada, National Aeronautical Establishment, YC. NRC, ME. Film No. 20, May 1969. Flow and sound visualization of an axisymmetric choked jet (24 in schlieren). (16 mm, silent film, running time 10 min).
-
(1969)
National Research Council of Canada, National Aeronautical Establishment, YC. NRC, ME. Film No. 20, May 1969
, vol.20
-
-
Westley, R.1
Woolley, J.H.2
-
22
-
-
0016521715
-
Discrete acoustic radiation from a high-speed jet as a singular perturbation problem
-
Y. Y. CHAN 1975 Canadian Aeronautics and Space Journal 21, 221-227. Discrete acoustic radiation from a high-speed jet as a singular perturbation problem.
-
(1975)
Canadian Aeronautics and Space Journal
, vol.21
, pp. 221-227
-
-
Chan, Y.Y.1
-
24
-
-
0040707513
-
The discrete component of the frequency spectrum of the noise of a free supersonic jet
-
A. V. RIMSKIY-KORSAKOV editor. Moscow: Nauka
-
T. Kh. SEDEL'NIKOV 1967 Physics of Aerodynamic Noise (A. V. RIMSKIY-KORSAKOV editor). Moscow: Nauka. The discrete component of the frequency spectrum of the noise of a free supersonic jet.
-
(1967)
Physics of Aerodynamic Noise
-
-
Sedel'nikov, T.Kh.1
-
25
-
-
0039522182
-
The frequency spectrum of the noise of a supersonic jet
-
A. V. RIMSKIY-KORSAKOV editor, Moscow: Nauka
-
T. Kh. SEDEL'NIKOV 1967 Physics of Aerodynamic Noise (A. V. RIMSKIY-KORSAKOV editor), Moscow: Nauka. The frequency spectrum of the noise of a supersonic jet.
-
(1967)
Physics of Aerodynamic Noise
-
-
Sedel'nikov, T.Kh.1
-
26
-
-
0040707502
-
The dispersion equations for multilayer jets and for several jets
-
A. V. RIMSKIY-KORSAKOV editor. Moscow: Nauka
-
T. Kh. SEDEL'NIKOV 1967 Physics of Aerodynamic Noise (A. V. RIMSKIY-KORSAKOV editor). Moscow: Nauka. The dispersion equations for multilayer jets and for several jets.
-
(1967)
Physics of Aerodynamic Noise
-
-
Sedel'nikov, T.Kh.1
-
27
-
-
0040707500
-
Discrete component in the noise spectrum of supersonic jets
-
V. M. ANUFRIEV, V. V. KOMAROV, V. M. KUPTSOV, D. A. MEL'NIKOV and A. A. SERGIENKO 1969 Izv. AN SSSR. Mekhanika Zhidkosti i Gaza 4, 162-165. Discrete component in the noise spectrum of supersonic jets.
-
(1969)
Izv. AN SSSR. Mekhanika Zhidkosti i Gaza
, vol.4
, pp. 162-165
-
-
Anufriev, V.M.1
Komarov, V.V.2
Kuptsov, V.M.3
Mel'nikov, D.A.4
Sergienko, A.A.5
-
28
-
-
0015626388
-
Some features of the propagation of a discrete tone perturbation in a free supersonic jet
-
V. N. GLAZNEV 1973 Fluid Mechanics Soviet Research 2, 76-79. Some features of the propagation of a discrete tone perturbation in a free supersonic jet.
-
(1973)
Fluid Mechanics Soviet Research
, vol.2
, pp. 76-79
-
-
Glaznev, V.N.1
-
30
-
-
0022525112
-
Experimental study of the space-time structure of fluctuations of pressure, velocity, and temperatures in gas flows at a discrete-tone frequency
-
V. N. GLAZNEV, V. S. DEMIN and Sh. SULEYMANOV 1986 Fluid Mechanics Soviet Research 15, 132-141. Experimental study of the space-time structure of fluctuations of pressure, velocity, and temperatures in gas flows at a discrete-tone frequency.
-
(1986)
Fluid Mechanics Soviet Research
, vol.15
, pp. 132-141
-
-
Glaznev, V.N.1
Demin, V.S.2
Suleymanov, Sh.3
-
31
-
-
0022815225
-
Interaction between a supersonic axisymmetric jet with a baffle or a countercurrent supersonic flow
-
Y. I. SOKOLOV and V. N. USKOV 1986 Fluid Mechanics Soviet Research 15, 16-35. Interaction between a supersonic axisymmetric jet with a baffle or a countercurrent supersonic flow.
-
(1986)
Fluid Mechanics Soviet Research
, vol.15
, pp. 16-35
-
-
Sokolov, Y.I.1
Uskov, V.N.2
-
43
-
-
0022787358
-
Dynamic loads on twin jet exhaust nozzles due to shock noise
-
T. D. NORUM and J. G. SHEARIN 1986 Journal of Aircraft 23, 728-729. Dynamic loads on twin jet exhaust nozzles due to shock noise.
-
(1986)
Journal of Aircraft
, vol.23
, pp. 728-729
-
-
Norum, T.D.1
Shearin, J.G.2
-
44
-
-
0002942882
-
The effects of nozzle exit lip thickness on plume resonance
-
M. K. PONTON and J. M. SEINER 1992 Journal of Sound and Vibration 154, 531-549. The effects of nozzle exit lip thickness on plume resonance.
-
(1992)
Journal of Sound and Vibration
, vol.154
, pp. 531-549
-
-
Ponton, M.K.1
Seiner, J.M.2
-
51
-
-
85030062798
-
Fluid mechanics of screech. A workstation tool, phase 2
-
A. B. CAIN, W. W. BOWER, R. H. BUSH and W. W. ROMER 1994 Contract final report, flight dynamics directorate, United States Air Force Wright Labs. Fluid mechanics of screech. A workstation tool, phase 2.
-
(1994)
Contract Final Report, Flight Dynamics Directorate, United States Air Force Wright Labs
-
-
Cain, A.B.1
Bower, W.W.2
Bush, R.H.3
Romer, W.W.4
-
55
-
-
0040707509
-
A note on the coupling between flow instabilities and incident sound
-
K. K. AHUJA and C. K. W. TAM 1982 Journal of Sound and Vibration 83, 433-439. A note on the coupling between flow instabilities and incident sound.
-
(1982)
Journal of Sound and Vibration
, vol.83
, pp. 433-439
-
-
Ahuja, K.K.1
Tam, C.K.W.2
-
57
-
-
85040502126
-
Basic experimental study of the coupling between flow instabilities and incident sound
-
K. K. AHUJA 1984 National Aeronautics and Space Administration CR 3789. Basic experimental study of the coupling between flow instabilities and incident sound.
-
(1984)
National Aeronautics and Space Administration CR 3789
-
-
Ahuja, K.K.1
-
60
-
-
0038929553
-
Acoustically excited heated jets, i-internal excitation
-
J. LEPICOVSKY, K. K AHUJA, W. H. BROWN, M. SALIKUDDIN and P. J. MORRIS 1988 National Aeronautics and Space Administration CR 4129. Acoustically excited heated jets, I-internal excitation.
-
(1988)
National Aeronautics and Space Administration CR 4129
-
-
Lepicovsky, J.1
Ahuja, K.K.2
Brown, W.H.3
Salikuddin, M.4
Morris, P.J.5
-
62
-
-
0024281474
-
A note on the effect of forward flight on shock-spacing in circular jets
-
P. J. MORRIS 1988 Journal of Sound and Vibration 122, 175-178. A note on the effect of forward flight on shock-spacing in circular jets.
-
(1988)
Journal of Sound and Vibration
, vol.122
, pp. 175-178
-
-
Morris, P.J.1
-
63
-
-
0024701990
-
A linear shock-cell model for jets of arbitrary exit geometry
-
P. J. MORRIS, T. R. S. BHAT and G. CHEN 1989 Journal of Sound and Vibration 132, 199-211. A linear shock-cell model for jets of arbitrary exit geometry.
-
(1989)
Journal of Sound and Vibration
, vol.132
, pp. 199-211
-
-
Morris, P.J.1
Bhat, T.R.S.2
Chen, G.3
-
64
-
-
0025521749
-
Instability waves in twin supersonic jets
-
P. J. MORRIS 1990 Journal of Fluid Mechanics 220, 293-307. Instability waves in twin supersonic jets.
-
(1990)
Journal of Fluid Mechanics
, vol.220
, pp. 293-307
-
-
Morris, P.J.1
-
65
-
-
0018493785
-
Noise generation instabilities in low reynolds number supersonic jets
-
G. L. MORRISON and D. K. MCLAUGHLIN 1979 Journal of Sound and Vibration 65, 177-191. Noise generation instabilities in low Reynolds number supersonic jets.
-
(1979)
Journal of Sound and Vibration
, vol.65
, pp. 177-191
-
-
Morrison, G.L.1
McLaughlin, D.K.2
-
66
-
-
0020098344
-
Experiments on the flow and acoustic properties of a moderate-Reynolds-number supersonic jet
-
T. R. TROUTT and D. K. MCLAUGHLIN 1982 Journal of Fluid Mechanics 116, 123-156. Experiments on the flow and acoustic properties of a moderate-Reynolds-number supersonic jet.
-
(1982)
Journal of Fluid Mechanics
, vol.116
, pp. 123-156
-
-
Troutt, T.R.1
McLaughlin, D.K.2
-
67
-
-
0025493370
-
Flow and acoustic properties of low reynolds number underexpanded supersonic jets
-
T. F. HU and D. K. MCLAUGHLIN 1990 Journal of Sound and Vibration 141, 485-505. Flow and acoustic properties of low Reynolds number underexpanded supersonic jets.
-
(1990)
Journal of Sound and Vibration
, vol.141
, pp. 485-505
-
-
Hu, T.F.1
McLaughlin, D.K.2
-
68
-
-
0022042964
-
A multiple-scales model of shock-cell structure of perfectly expanded supersonic jets
-
C. K. W. TAM, J. A. JACKSON and J. M. SEINER 1985 Journal of Fluid Mechanics 153, 123-149. A multiple-scales model of shock-cell structure of perfectly expanded supersonic jets.
-
(1985)
Journal of Fluid Mechanics
, vol.153
, pp. 123-149
-
-
Tam, C.K.W.1
Jackson, J.A.2
Seiner, J.M.3
-
69
-
-
0022794738
-
Proposed relationship between broadband shock associated noise and screech tones
-
C. K. W. TAM, J. M. SEINER and J. C. YU 1986 Journal of Sound and Vibration 110, 309-321. Proposed relationship between broadband shock associated noise and screech tones.
-
(1986)
Journal of Sound and Vibration
, vol.110
, pp. 309-321
-
-
Tam, C.K.W.1
Seiner, J.M.2
Yu, J.C.3
-
70
-
-
38249042141
-
Excitation of instability waves by sound - A physical interpretation
-
C. K. W. TAM 1986 Journal of Sound and Vibration 105, 169-172. Excitation of instability waves by sound - a physical interpretation.
-
(1986)
Journal of Sound and Vibration
, vol.105
, pp. 169-172
-
-
Tam, C.K.W.1
-
72
-
-
0023963043
-
The shock-cell structures and screech tone frequencies of rectangular and non-axisymmetric supersonic jets
-
C. K. W. TAM 1988 Journal of Sound and Vibration 121, 135-147. The shock-cell structures and screech tone frequencies of rectangular and non-axisymmetric supersonic jets.
-
(1988)
Journal of Sound and Vibration
, vol.121
, pp. 135-147
-
-
Tam, C.K.W.1
-
73
-
-
0000950698
-
Jet noise generated by large-scale coherent motion, aeroacoustics of flight vehicles: Theory and practice, Vol. 1: Noise sources
-
H. H. Hubbard, editor
-
C. K. W. TAM 1991 National Aeronautics and Space Administration RP 1258, WRDC TR C90-3052, (H. H. Hubbard, editor), 311-390. Jet noise generated by large-scale coherent motion, aeroacoustics of flight vehicles: theory and practice, Vol. 1: noise sources.
-
(1991)
National Aeronautics and Space Administration RP 1258, WRDC TR C90-3052
, pp. 311-390
-
-
Tam, C.K.W.1
-
79
-
-
0003322210
-
Flight effects on the far-field noise of a heated supersonic jet
-
A. KROTHAPALLI, P. T. SODERMAN, C. S. ALLEN, J. A. HAYES and S. M. JAEGER 1997 American Institute of Aeronautics and Astronautics Journal 35, 952-957. Flight effects on the far-field noise of a heated supersonic jet.
-
(1997)
American Institute of Aeronautics and Astronautics Journal
, vol.35
, pp. 952-957
-
-
Krothapalli, A.1
Soderman, P.T.2
Allen, C.S.3
Hayes, J.A.4
Jaeger, S.M.5
-
82
-
-
0025474153
-
Twin-jet screech suppression
-
L. SHAW 1990 Journal of Aircraft, 27, 708-715. Twin-jet screech suppression.
-
(1990)
Journal of Aircraft
, vol.27
, pp. 708-715
-
-
Shaw, L.1
-
83
-
-
0040707501
-
Twin jet screech suppression concepts tested for 4-7% axisymmetric and two-dimensional nozzle configurations
-
S. WALKER 1990 American Institute of Aeronautics and Astronautics Paper 90-2150. Twin jet screech suppression concepts tested for 4-7% axisymmetric and two-dimensional nozzle configurations.
-
(1990)
American Institute of Aeronautics and Astronautics Paper 90-2150
-
-
Walker, S.1
-
84
-
-
0001425399
-
A wavelet transform analysis applied to unsteady aspects of supersonic jet screech resonance
-
S. H. WALKER, S. V. GORDEYEV and F. O. THOMAS 1997 Experiments in Fluids 22, 229-238. A Wavelet transform analysis applied to unsteady aspects of supersonic jet screech resonance.
-
(1997)
Experiments in Fluids
, vol.22
, pp. 229-238
-
-
Walker, S.H.1
Gordeyev, S.V.2
Thomas, F.O.3
-
85
-
-
0031238112
-
Experiments characterizing nonlinear shear layer dynamics in a supersonic rectangular jet undergoing screech
-
S. H. WALKER and F. O. THOMAS 1997 Physics of Fluids 9, 2562-2579. Experiments characterizing nonlinear shear layer dynamics in a supersonic rectangular jet undergoing screech.
-
(1997)
Physics of Fluids
, vol.9
, pp. 2562-2579
-
-
Walker, S.H.1
Thomas, F.O.2
-
86
-
-
0012534995
-
Initial turbulence effect on jet evolution with and without tonal excitation
-
G. RAMAN, K. B. M. Q. ZAMAN and E. J. RICE 1989 Physics of Fluids A1, 1240-1248. Initial turbulence effect on jet evolution with and without tonal excitation.
-
(1989)
Physics of Fluids
, vol.A1
, pp. 1240-1248
-
-
Raman, G.1
Zaman, K.B.M.Q.2
Rice, E.J.3
-
88
-
-
0027962835
-
Instability modes excited by natural screech tones in a supersonic rectangular jet
-
G. RAMAN and E. J. RICE 1994 Physics of Fluids 6, 3999-4008. Instability modes excited by natural screech tones in a supersonic rectangular jet.
-
(1994)
Physics of Fluids
, vol.6
, pp. 3999-4008
-
-
Raman, G.1
Rice, E.J.2
-
89
-
-
85030070286
-
Lewis data provided to McDonnell Douglas Aerospace as a part of the U.S. Air Force screech cooperative program
-
G. RAMAN 1995 National Aeronautics and Space Administration. Lewis data provided to McDonnell Douglas Aerospace as a part of the U.S. Air Force screech cooperative program.
-
(1995)
National Aeronautics and Space Administration
-
-
Raman, G.1
-
90
-
-
0029257007
-
Supersonic jet mixing enhancement using impingement tones from obstacles of various geometries
-
G. RAMAN and E. J. RICE 1995 American Institute of Aeronautics and Astronautics Journal 33, 454-462. Supersonic jet mixing enhancement using impingement tones from obstacles of various geometries.
-
(1995)
American Institute of Aeronautics and Astronautics Journal
, vol.33
, pp. 454-462
-
-
Raman, G.1
Rice, E.J.2
-
91
-
-
0030087299
-
Resonant interaction of a linear array of supersonic rectangular jets: An experimental study
-
and Corrigendum 326, 1996, 437.
-
G. RAMAN and R. TAGHAVI 1996 Journal of Fluid Mechanics 309, 93-111 (and Corrigendum 326, 1996, 437). Resonant interaction of a linear array of supersonic rectangular jets: an experimental study.
-
(1996)
Journal of Fluid Mechanics
, vol.309
, pp. 93-111
-
-
Raman, G.1
Taghavi, R.2
-
92
-
-
0031122212
-
Cessation of screech in underexpanded jets
-
G. RAMAN 1997 Journal of Fluid Mechanics 336, 69-90. Cessation of screech in underexpanded jets.
-
(1997)
Journal of Fluid Mechanics
, vol.336
, pp. 69-90
-
-
Raman, G.1
-
93
-
-
0030784311
-
Screech tones from rectangular jets with spanwise oblique shock-cell structures
-
G. RAMAN 1997 Journal of Fluid Mechanics 330, 141-168. Screech tones from rectangular jets with spanwise oblique shock-cell structures.
-
(1997)
Journal of Fluid Mechanics
, vol.330
, pp. 141-168
-
-
Raman, G.1
-
95
-
-
0031678524
-
Coupling of twin supersonic rectangular jets
-
G. RAMAN and R. TAGHAVI 1998 Journal of Fluid Mechanics 354, 123-146. Coupling of twin supersonic rectangular jets.
-
(1998)
Journal of Fluid Mechanics
, vol.354
, pp. 123-146
-
-
Raman, G.1
Taghavi, R.2
-
99
-
-
0004891360
-
Mixing noise reduction for rectangular supersonic jets by nozzle shaping and induced screech mixing
-
also National Aeronautics and Space Administration TM 106364
-
E. J. RICE and G. RAMAN 1993 American Institute of Aeronautics and Astronautics Paper 93-4322 (also National Aeronautics and Space Administration TM 106364). Mixing noise reduction for rectangular supersonic jets by nozzle shaping and induced screech mixing.
-
(1993)
American Institute of Aeronautics and Astronautics Paper 93-4322
-
-
Rice, E.J.1
Raman, G.2
-
102
-
-
0006175883
-
-
U. S. Patents 5, 325, 661, and 5, 392, 597
-
E. J. RICE 1995 U. S. Patents 5, 325, 661, and 5, 392, 597. Jet mixer noise suppressor using acoustic feedback.
-
(1995)
Jet Mixer Noise Suppressor Using Acoustic Feedback
-
-
Rice, E.J.1
-
107
-
-
84967850154
-
The sound producing oscillations of round underexpanded jets impinging on normal plates
-
A. POWELL 1988 Journal of the Acoustical Society of America 83, 515-533. The sound producing oscillations of round underexpanded jets impinging on normal plates.
-
(1988)
Journal of the Acoustical Society of America
, vol.83
, pp. 515-533
-
-
Powell, A.1
-
109
-
-
0025914012
-
A note on the cell length of noncircular supersonic jets
-
A. POWELL 1991 Journal of the Acoustical Society of America 89, 3004-3006. A note on the cell length of noncircular supersonic jets.
-
(1991)
Journal of the Acoustical Society of America
, vol.89
, pp. 3004-3006
-
-
Powell, A.1
-
112
-
-
0028835483
-
The focal phase shift of waves of a circular membrane, applied to underexpanded supersonic jet structure
-
A. POWELL 1995 Journal of the Acoustical Society of America 97, 927-932. The focal phase shift of waves of a circular membrane, applied to underexpanded supersonic jet structure.
-
(1995)
Journal of the Acoustical Society of America
, vol.97
, pp. 927-932
-
-
Powell, A.1
-
114
-
-
0030795079
-
Symmetrical oscillation modes in choked-jet edge tones and screech from rectangular nozzles
-
D. LIN and A. POWELL 1997 Journal of the Acoustical Society of America 102, 1235-1238. Symmetrical oscillation modes in choked-jet edge tones and screech from rectangular nozzles.
-
(1997)
Journal of the Acoustical Society of America
, vol.102
, pp. 1235-1238
-
-
Lin, D.1
Powell, A.2
-
118
-
-
0039522178
-
Instability of astrophysical jets. II. Numerical simulation of two-dimensional underexpanded slab jets
-
Y. UMEDA and A. YASUDA 1990 Progress in Theoretical Physics 84, 856-866. Instability of astrophysical jets. II. Numerical simulation of two-dimensional underexpanded slab jets.
-
(1990)
Progress in Theoretical Physics
, vol.84
, pp. 856-866
-
-
Umeda, Y.1
Yasuda, A.2
-
119
-
-
0028218516
-
Oscillation modes of underexpanded jets issuing from square and equilateral triangular nozzles
-
Y. UMEDA and R. ISHII 1994 Journal of the Acoustical Society of America 95, 1853-1857. Oscillation modes of underexpanded jets issuing from square and equilateral triangular nozzles.
-
(1994)
Journal of the Acoustical Society of America
, vol.95
, pp. 1853-1857
-
-
Umeda, Y.1
Ishii, R.2
-
120
-
-
0029427243
-
Oscillation modes of supersonic multi-jet
-
G. RAMAN, S. KAJI, C. J. FREITAS, editors
-
Y. UMEDA and R. ISHII 1995 American Society of Mechanical Engineers, FED-Vol. 214, High Speed Jet Flows (G. RAMAN, S. KAJI, C. J. FREITAS, editors), 151-156. Oscillation modes of supersonic multi-jet.
-
(1995)
American Society of Mechanical Engineers, FED-Vol. 214, High Speed Jet Flows
, vol.214
, pp. 151-156
-
-
Umeda, Y.1
Ishii, R.2
-
121
-
-
0029423110
-
Numerical studies of noise generation and mixing of supersonic rectangular jets
-
G. RAMAN, S. KAJI, and C. J. FREITAS, editors. ASME, NY
-
R. KOLBE, K. KAILASANATH, T. YOUNG and J. BORIS 1995 American Society of Mechanical Engineers, FED-Vol. 214, High Speed Jet Flows (G. RAMAN, S. KAJI, and C. J. FREITAS, editors). ASME, NY, 41-46. Numerical studies of noise generation and mixing of supersonic rectangular jets.
-
(1995)
American Society of Mechanical Engineers, FED-Vol. 214, High Speed Jet Flows
, vol.214
, pp. 41-46
-
-
Kolbe, R.1
Kailasanath, K.2
Young, T.3
Boris, J.4
-
122
-
-
0038929556
-
Numerical simulations of flow modification of supersonic rectangular jets
-
R. KOLBE, K. KAILASANATH, T. YOUNG, J. BORIS and A. LANDSBERG 1996 American Institute of Aeronautics and Astronautics Journal 34, 902-908. Numerical simulations of flow modification of supersonic rectangular jets.
-
(1996)
American Institute of Aeronautics and Astronautics Journal
, vol.34
, pp. 902-908
-
-
Kolbe, R.1
Kailasanath, K.2
Young, T.3
Boris, J.4
Landsberg, A.5
-
123
-
-
0030718354
-
A comparison of numerical simulations to experiments on supersonic rectangular jets
-
American Society of Mechanical Engineers Fluids Engineering Meeting, Vancouver, Canada
-
R. L. KOLBE, K. KAILASANATH, J. P. BORIS and G. RAMAN 1997 American Society of Mechanical Engineers Paper FEDSM497-3235, American Society of Mechanical Engineers Fluids Engineering Meeting, Vancouver, Canada. A comparison of numerical simulations to experiments on supersonic rectangular jets.
-
(1997)
American Society of Mechanical Engineers Paper FEDSM497-3235
-
-
Kolbe, R.L.1
Kailasanath, K.2
Boris, J.P.3
Raman, G.4
-
126
-
-
0031599141
-
Advances in understanding supersonic jet screech: Review and perspective
-
G. RAMAN 1998 Progress in Aerospace Science 34, 45-106. Advances in understanding supersonic jet screech: review and perspective.
-
(1998)
Progress in Aerospace Science
, vol.34
, pp. 45-106
-
-
Raman, G.1
-
128
-
-
0006098223
-
A note on prandtl's formula for the wavelength of a supersonic gas jet
-
D. C. PACK 1950 Quarterly Journal of Mechanics and Applied Mathematics 3, 173-181. A note on Prandtl's formula for the wavelength of a supersonic gas jet.
-
(1950)
Quarterly Journal of Mechanics and Applied Mathematics
, vol.3
, pp. 173-181
-
-
Pack, D.C.1
-
131
-
-
0009720753
-
The puzzle of whip cracking - Uncovered by a correlation of whip-tip kinematics with shock wave emission
-
P. KREHL, S. ENGEMANN and D. SCHWENKEL 1998 Shock Waves, 8, 1-9. The puzzle of whip cracking - uncovered by a correlation of whip-tip kinematics with shock wave emission.
-
(1998)
Shock Waves
, vol.8
, pp. 1-9
-
-
Krehl, P.1
Engemann, S.2
Schwenkel, D.3
-
134
-
-
0040544035
-
An investigation of the noise field from a small jet and methods for its reduction
-
England
-
R. WESTLEY and G. M. LILLEY 1952 Rep. No. 53, College of Aeronautics, Cranfield (England). An investigation of the noise field from a small jet and methods for its reduction.
-
(1952)
Rep. No. 53, College of Aeronautics, Cranfield
, vol.53
-
-
Westley, R.1
Lilley, G.M.2
-
136
-
-
0003711047
-
-
Cambridge: Cambridge University Press
-
M. J. T. SMITH 1989 Aircraft Noise. Cambridge: Cambridge University Press.
-
(1989)
Aircraft Noise
-
-
Smith, M.J.T.1
-
137
-
-
0012233298
-
Jet noise classical theory and experiments
-
H. H. Hubbard, editor
-
G. M. LILLEY 1991 Aeroacoustics of Flight Vehicles, Theory and Practice, Vol. 1: Noise Sources, National Aeronautics and Space Administration RP-1258, WRDC, TR-90-3052, (H. H. Hubbard, editor), 211-289. Jet noise classical theory and experiments.
-
(1991)
Aeroacoustics of Flight Vehicles, Theory and Practice, Vol. 1: Noise Sources, National Aeronautics and Space Administration RP-1258, WRDC, TR-90-3052
, vol.1
, pp. 211-289
-
-
Lilley, G.M.1
-
139
-
-
0031553021
-
A study of screech tone noise of supersonic swirling jets
-
Y. K. YU and R. H. CHEN 1997 Journal of Sound and Vibration 205, 698-705. A study of screech tone noise of supersonic swirling jets.
-
(1997)
Journal of Sound and Vibration
, vol.205
, pp. 698-705
-
-
Yu, Y.K.1
Chen, R.H.2
-
141
-
-
0022809042
-
The design and optimization of propulsion systems employing scarfed nozzles
-
J. S. LILLEY 1986 Journal of Spacecraft and Rockets 23, 597-604. The design and optimization of propulsion systems employing scarfed nozzles.
-
(1986)
Journal of Spacecraft and Rockets
, vol.23
, pp. 597-604
-
-
Lilley, J.S.1
-
144
-
-
0000110760
-
The oscillation and noise of an overpressure sonic jet
-
A. G. HAMMITT 1961 Journal of Aeronautical Science 28, 673-680. The oscillation and noise of an overpressure sonic jet.
-
(1961)
Journal of Aeronautical Science
, vol.28
, pp. 673-680
-
-
Hammitt, A.G.1
-
146
-
-
84980068276
-
Šber die beim ausstromen det luft entstehenden tone
-
SONDHAUSS 1854 Annalen der Physik, Leipzig 91, 126-147, 214-240. šber die beim Ausstromen det Luft entstehenden Tone.
-
(1854)
Annalen der Physik, Leipzig
, vol.91
, pp. 126-147
-
-
Sondhauss1
-
148
-
-
84972054357
-
The edge-tone feedback cycle; linear theory for the operating stages
-
D. G. CRIGHTON 1992 Journal of Fluid Mechanics 234, 361-391. The edge-tone feedback cycle; linear theory for the operating stages.
-
(1992)
Journal of Fluid Mechanics
, vol.234
, pp. 361-391
-
-
Crighton, D.G.1
-
149
-
-
0027912582
-
Experiments concerning tones produced by an axisymmetric choked jet impinging on flat plates
-
B. HENDERSON and A. POWELL 1993 Journal of Sound and Vibration 168, 307-326. Experiments concerning tones produced by an axisymmetric choked jet impinging on flat plates.
-
(1993)
Journal of Sound and Vibration
, vol.168
, pp. 307-326
-
-
Henderson, B.1
Powell, A.2
-
150
-
-
0030052542
-
Sound-production mechanisms of the axisymmetric choked jet impinging on small plates: The production of primary tones
-
B. HENDERSON and A. POWELL 1996 Journal of the Acoustical Society of America 99, 153-162. Sound-production mechanisms of the axisymmetric choked jet impinging on small plates: the production of primary tones.
-
(1996)
Journal of the Acoustical Society of America
, vol.99
, pp. 153-162
-
-
Henderson, B.1
Powell, A.2
-
151
-
-
0039522173
-
Necessary conditions for starting and maintaining a stable oscillatory flow in a hartmann-sprenger tube
-
J. IWAMOTO 1986 Flow Visualization, 4, 507-512. Necessary conditions for starting and maintaining a stable oscillatory flow in a Hartmann-Sprenger tube.
-
(1986)
Flow Visualization
, vol.4
, pp. 507-512
-
-
Iwamoto, J.1
-
152
-
-
0039685160
-
Experimental study of flow oscillation in a rectangular jet-driven tube
-
J. IWAMOTO 1990 ASME Journal of Fluids Engineering, 112, 23-27. Experimental study of flow oscillation in a rectangular jet-driven tube.
-
(1990)
ASME Journal of Fluids Engineering
, vol.112
, pp. 23-27
-
-
Iwamoto, J.1
|