-
1
-
-
0842268987
-
Calculation of sound propagating in nonuniform flows: Suppression of instability waves
-
Agarwal A, Morris PJ, Mani R. 2004. Calculation of sound propagating in nonuniform flows: suppression of instability waves. AIAA J. 42(1):80-88
-
(2004)
AIAA J.
, vol.42
, Issue.1
, pp. 80-88
-
-
Agarwal, A.1
Morris, P.J.2
Mani, R.3
-
2
-
-
0033078117
-
Calculation of basic sound radiation of axisymmetric jets by direct numerical simulations
-
Avital EJ, Sandham ND, Luo KH. 1999. Calculation of basic sound radiation of axisymmetric jets by direct numerical simulations. AIAA J. 37(2):161-68
-
(1999)
AIAA J.
, vol.37
, Issue.2
, pp. 161-168
-
-
Avital, E.J.1
Sandham, N.D.2
Luo, K.H.3
-
3
-
-
0001754587
-
Subsonic and supersonic jet noise predictions from statistical source models
-
Bailly C, Lafon P, Candel S. 1997. Subsonic and supersonic jet noise predictions from statistical source models. AIAA J. 35(11):1688-96
-
(1997)
AIAA J.
, vol.35
, Issue.11
, pp. 1688-1696
-
-
Bailly, C.1
Lafon, P.2
Candel, S.3
-
4
-
-
0003550982
-
Improved turbulence models based on large-eddy simulation of homogeneous, incompressible, turbulent flows
-
Tech. Rep. TF-19, Dep. Mech. Eng., Stanford Univ., Stanford, CA
-
Bardina J, Ferziger J, Reynolds WC. 1983. Improved turbulence models based on large-eddy simulation of homogeneous, incompressible, turbulent flows. Tech. Rep. TF-19, Dep. Mech. Eng., Stanford Univ., Stanford, CA
-
(1983)
-
-
Bardina, J.1
Ferziger, J.2
Reynolds, W.C.3
-
5
-
-
0031098453
-
Computation of jet mixing noise due to coherent structures: The plan jet case
-
Bastin F, Lafon P, Candel S. 1997. Computation of jet mixing noise due to coherent structures: the plan jet case. J. Fluid Mech. 335:261-304
-
(1997)
J. Fluid Mech.
, vol.335
, pp. 261-304
-
-
Bastin, F.1
Lafon, P.2
Candel, S.3
-
6
-
-
0005708523
-
A statistical description of pressure and velocity fields at the trailing edge of a flat strut
-
Tech. Rep. No. 4241, David Taylor Naval Ship Res. Dev. Cent., Bethesda, MD
-
Blake WK. 1975. A statistical description of pressure and velocity fields at the trailing edge of a flat strut. Tech. Rep. No. 4241, David Taylor Naval Ship Res. Dev. Cent., Bethesda, MD
-
(1975)
-
-
Blake, W.K.1
-
8
-
-
0142112891
-
The aeroacoustics of trailing edges
-
ed. M Gad-el-Hak, New York. Springer-Verlag. 532 pp
-
Blake WK, Gershfeld JL. 1988. The aeroacoustics of trailing edges. In Frontiers in Experimental Fluid Mechanics, ed. M Gad-el-Hak, pp. 457-532. New York. Springer-Verlag. 532 pp.
-
(1988)
Frontiers in Experimental Fluid Mechanics
, pp. 457-532
-
-
Blake, W.K.1
Gershfeld, J.L.2
-
9
-
-
29244465765
-
Aeroacoustic prediction of turbulent free shear flows
-
PhD thesis. Dep. Aeronaut. Astronaut., Stanford Univ., Stanford, CA
-
Bodony DJ. 2004. Aeroacoustic prediction of turbulent free shear flows. PhD thesis. Dep. Aeronaut. Astronaut., Stanford Univ., Stanford, CA
-
(2004)
-
-
Bodony, D.J.1
-
10
-
-
85087187931
-
A statistical subgrid scale noise model: Formulation
-
AIAA/CEAS Pap. 2003-3252
-
Bodony DJ, Lele SK. 2003. A statistical subgrid scale noise model: formulation. AIAA/CEAS Pap. 2003-3252
-
(2003)
-
-
Bodony, D.J.1
Lele, S.K.2
-
11
-
-
24144442176
-
On using large-eddy simulation for the prediction of noise from cold and heated turbulent jets
-
Bodony DJ, Lele SK. 2005. On using large-eddy simulation for the prediction of noise from cold and heated turbulent jets. Phys. Fluids. 17(8):085103
-
(2005)
Phys. Fluids.
, vol.17
, Issue.8
, pp. 085103
-
-
Bodony, D.J.1
Lele, S.K.2
-
12
-
-
18944400888
-
Effects of inflow conditions and forcing on subsonic jet flows and noise
-
Bogey C, Bailly C. 2005a. Effects of inflow conditions and forcing on subsonic jet flows and noise. AIAA J. 43:1000-7
-
(2005)
AIAA J.
, vol.43
, pp. 1000-1007
-
-
Bogey, C.1
Bailly, C.2
-
13
-
-
13444270437
-
Decrease of the effective Reynolds number with eddy-viscosity subgrid-scale modeling
-
Bogey C, Bailly C. 2005b. Decrease of the effective Reynolds number with eddy-viscosity subgrid-scale modeling. AIAA J. 43:437-39
-
(2005)
AIAA J.
, vol.43
, pp. 437-439
-
-
Bogey, C.1
Bailly, C.2
-
14
-
-
0036472045
-
Computation of flow noise using source terms in linearized Euler's equations
-
Bogey C, Bailly C, Juvé D. 2002. Computation of flow noise using source terms in linearized Euler's equations. AIAA J. 40(2):235-43
-
(2002)
AIAA J.
, vol.40
, Issue.2
, pp. 235-243
-
-
Bogey, C.1
Bailly, C.2
Juvé, D.3
-
15
-
-
0037360678
-
Noise investigation of a high subsonic, moderate Reynolds number jet using a compressible large eddy simulation
-
Bogey C, Bailly C, Juvé D. 2003. Noise investigation of a high subsonic, moderate Reynolds number jet using a compressible large eddy simulation. Theor Comput. Fluid Dyn. 16(4):273-97
-
(2003)
Theor Comput. Fluid Dyn.
, vol.16
, Issue.4
, pp. 273-297
-
-
Bogey, C.1
Bailly, C.2
Juvé, D.3
-
16
-
-
0033077012
-
A rigorous framework for optimization of expensive functions by surrogates
-
Booker AJ, Dennis JE, Frank PD, Serafini DB, Torczon V, Trosset MW. 1999. A rigorous framework for optimization of expensive functions by surrogates. Struct. Optim. 17(1):1-13
-
(1999)
Struct. Optim.
, vol.17
, Issue.1
, pp. 1-13
-
-
Booker, A.J.1
Dennis, J.E.2
Frank, P.D.3
Serafini, D.B.4
Torczon, V.5
Trosset, M.W.6
-
17
-
-
0000950129
-
An analytical comparison of the acoustic analogy and Kirchhoff formulation for moving surfaces
-
Brentner KS, Farassat F. 1998. An analytical comparison of the acoustic analogy and Kirchhoff formulation for moving surfaces. AIAA J. 36(8):1379-86
-
(1998)
AIAA J.
, vol.36
, Issue.8
, pp. 1379-1386
-
-
Brentner, K.S.1
Farassat, F.2
-
18
-
-
0037294895
-
Modeling aerodynamically generated sound of helicopter rotors
-
Brentner KS, Farassat F. 2003. Modeling aerodynamically generated sound of helicopter rotors. Prog. Aerospace Sci. 39(2-3):83-120
-
(2003)
Prog. Aerospace Sci.
, vol.39
, Issue.2-3
, pp. 83-120
-
-
Brentner, K.S.1
Farassat, F.2
-
19
-
-
84896690319
-
Turbulence measurements of separated flow nozzles with mixing enhancement features
-
AIAA Pap. 2002-2484
-
Bridges J, Wernet MP. 2002. Turbulence measurements of separated flow nozzles with mixing enhancement features. AIAA Pap. 2002-2484
-
(2002)
-
-
Bridges, J.1
Wernet, M.P.2
-
20
-
-
0033682257
-
Approximate wall boundary conditions in the large-eddy simulation of high Reynolds number flow
-
Cabot WH, Moin P. 2000. Approximate wall boundary conditions in the large-eddy simulation of high Reynolds number flow. Flow Turb. Combust. 63(1-4):269-91
-
(2000)
Flow Turb. Combust.
, vol.63
, Issue.1-4
, pp. 269-291
-
-
Cabot, W.H.1
Moin, P.2
-
21
-
-
84860940029
-
Non-linear interactions in a viscous heat-conducting compressible gas
-
Chu BT, Kovásznay LSG. 1958. Non-linear interactions in a viscous heat-conducting compressible gas. J. Fluid Mech. 3:494-514
-
(1958)
J. Fluid Mech.
, vol.3
, pp. 494-514
-
-
Chu, B.T.1
Kovásznay, L.S.G.2
-
22
-
-
0012547952
-
Optimal control of aeroacoustic noise generated by cylinder vortex interaction
-
Collis SS, Ghayour K, Heinkenschloss M. 2002. Optimal control of aeroacoustic noise generated by cylinder vortex interaction. Int. J. Aeroacoustics 1(2):97-114
-
(2002)
Int. J. Aeroacoustics
, vol.1
, Issue.2
, pp. 97-114
-
-
Collis, S.S.1
Ghayour, K.2
Heinkenschloss, M.3
-
23
-
-
1642380534
-
Modeling artificial boundary conditions for compressible flow
-
Colonius T. 2004. Modeling artificial boundary conditions for compressible flow. Annu. Rev. Fluid Mech. 36:315-45
-
(2004)
Annu. Rev. Fluid Mech.
, vol.36
, pp. 315-345
-
-
Colonius, T.1
-
24
-
-
0034140974
-
Application of Lighthill's equation to a Mach 1.92 turbulent jet
-
Colonius T, Freund JB. 2000. Application of Lighthill's equation to a Mach 1.92 turbulent jet. AIAA J. 38(2):368-70
-
(2000)
AIAA J.
, vol.38
, Issue.2
, pp. 368-370
-
-
Colonius, T.1
Freund, J.B.2
-
25
-
-
9944264070
-
Computational aeroacoustics: Progress on nonlinear problems of sound generation
-
Colonius T, Lele SK, 2004. Computational aeroacoustics: progress on nonlinear problems of sound generation. Prog. Aerospace Sci. 40(6):345-416
-
(2004)
Prog. Aerospace Sci.
, vol.40
, Issue.6
, pp. 345-416
-
-
Colonius, T.1
Lele, S.K.2
-
27
-
-
0016474762
-
Basic principles of aerodynamic noise generation
-
Crighton DG. 1975. Basic principles of aerodynamic noise generation. Prog. Aerospace Sci. 16(1):31-96
-
(1975)
Prog. Aerospace Sci.
, vol.16
, Issue.1
, pp. 31-96
-
-
Crighton, D.G.1
-
28
-
-
0345069374
-
Goals for computational aeroacoustics
-
ed. D Lee, RL Sternberg, MH Schultz, Amsterdam: Elsevier-North Holland
-
Crighton DG. 1988. Goals for computational aeroacoustics. In Computational Acoustics. Algorithms and Applications, ed. D Lee, RL Sternberg, MH Schultz, pp. 3-20. Amsterdam: Elsevier-North Holland
-
(1988)
Computational Acoustics: Algorithms and Applications
, pp. 3-20
-
-
Crighton, D.G.1
-
29
-
-
0004639573
-
Computational aeroacoustics for low Mach number flows
-
ed. JC Hardin, MY Hussaini, New York Springer-Verlag. 513 pp
-
Crighton DG. 1993. Computational aeroacoustics for low Mach number flows. In Computational Aeroacoustics, ed. JC Hardin, MY Hussaini, pp. 50-68. New York Springer-Verlag. 513 pp.
-
(1993)
Computational Aeroacoustics
, pp. 50-68
-
-
Crighton, D.G.1
-
30
-
-
0003695977
-
-
New York: Springer-Verlag
-
Crighton DG, Dowling AP, Ffowes Williams JE, Heckl M, Leppington FG. 1992. Modern Methods in Analytical Acoustics. New York: Springer-Verlag. 738 pp.
-
(1992)
Modern Methods in Analytical Acoustics
, pp. 738
-
-
Crighton, D.G.1
Dowling, A.P.2
Ffowes Williams, J.E.3
Heckl, M.4
Leppington, F.G.5
-
31
-
-
0014747025
-
Aerodynamic sound emission as a singular perturbation problem
-
Crow SC. 1970. Aerodynamic sound emission as a singular perturbation problem. Stud. Appl. Math. 49(1):1-44
-
(1970)
Stud. Appl. Math.
, vol.49
, Issue.1
, pp. 1-44
-
-
Crow, S.C.1
-
32
-
-
0001514172
-
The influence of solid boundaries upon aerodynamic sound
-
Curle N. 1955. The influence of solid boundaries upon aerodynamic sound. Proc. R. Soc. London Ser. A 231(1187):505-14
-
(1955)
Proc. R. Soc. London Ser. A
, vol.231
, Issue.1187
, pp. 505-514
-
-
Curle, N.1
-
33
-
-
0014767004
-
A numerical study of three-dimensional turbulent channel flow at large Reynolds numbers
-
Deardorff JW. 1970. A numerical study of three-dimensional turbulent channel flow at large Reynolds numbers. J. Fluid Mech. 41:453-80
-
(1970)
J. Fluid Mech.
, vol.41
, pp. 453-480
-
-
Deardorff, J.W.1
-
34
-
-
0004700663
-
Analysis of internally generated sound in continuous materials: 2. A critical review of the conceptual adequacy and physical scope of existing theories of aerodynamic noise, with special reference to supersonic jet noise
-
Doak PE. 1972. Analysis of internally generated sound in continuous materials: 2. A critical review of the conceptual adequacy and physical scope of existing theories of aerodynamic noise, with special reference to supersonic jet noise. J. Sound Vib. 25(2):263-335
-
(1972)
J. Sound Vib.
, vol.25
, Issue.2
, pp. 263-335
-
-
Doak, P.E.1
-
35
-
-
0017299921
-
Convective amplification of real simple sources
-
Dowling A. 1976. Convective amplification of real simple sources. J. Fluid Mech. 74(3):529-46
-
(1976)
J. Fluid Mech.
, vol.74
, Issue.3
, pp. 529-546
-
-
Dowling, A.1
-
36
-
-
0024034759
-
Extension of Kirchhoffs formula to radiation from moving surfaces
-
Farassat F, Myers MK. 1988. Extension of Kirchhoffs formula to radiation from moving surfaces. J. Sound Vib. 123(3):451-61
-
(1988)
J. Sound Vib.
, vol.123
, Issue.3
, pp. 451-461
-
-
Farassat, F.1
Myers, M.K.2
-
38
-
-
0014937763
-
Aerodynamic sound generation by turbulent flow in the vicinity of a scattering half plane
-
Ffowcs Williams JE, Hall LH. 1970. Aerodynamic sound generation by turbulent flow in the vicinity of a scattering half plane. J. Fluid Mech. 40:657-70
-
(1970)
J. Fluid Mech.
, vol.40
, pp. 657-670
-
-
Ffowcs Williams, J.E.1
Hall, L.H.2
-
40
-
-
0000977285
-
A proposed inflow/outflow boundary condition for direct computation of aerodynamic sound
-
Freund JB. 1997. A proposed inflow/outflow boundary condition for direct computation of aerodynamic sound. AIAA J. 35(4):740-42
-
(1997)
AIAA J.
, vol.35
, Issue.4
, pp. 740-742
-
-
Freund, J.B.1
-
41
-
-
0035838521
-
Noise sources in a low-Reynolds-number turbulent jet at Mach 0.9
-
Freund JB. 2001. Noise sources in a low-Reynolds-number turbulent jet at Mach 0.9. J. Fluid Mech. 438:277-305
-
(2001)
J. Fluid Mech.
, vol.438
, pp. 277-305
-
-
Freund, J.B.1
-
42
-
-
0037830968
-
Noise-source turbulence statistics and the noise from a Mach 0.9 jet
-
Freund JB. 2003. Noise-source turbulence statistics and the noise from a Mach 0.9 jet. Phys. Fluids 15(6):1788-99
-
(2003)
Phys. Fluids
, vol.15
, Issue.6
, pp. 1788-1799
-
-
Freund, J.B.1
-
43
-
-
0003609011
-
POD analysis of sound generation by a turbulent jet
-
AIAA Pap. 2002-0072
-
Freund JB, Colonius T. 2002. POD analysis of sound generation by a turbulent jet. AIAA Pap. 2002-0072
-
(2002)
-
-
Freund, J.B.1
Colonius, T.2
-
45
-
-
0004176433
-
Calculation of the radiated sound field using an open Kirchhoff surface
-
Freund JB, Lele SK., Moin P. 1996. Calculation of the radiated sound field using an open Kirchhoff surface. AIAA J. 34(5):909-16
-
(1996)
AIAA J.
, vol.34
, Issue.5
, pp. 909-916
-
-
Freund, J.B.1
Lele, S.K.2
Moin, P.3
-
46
-
-
0034321712
-
Direct numerical simulation of a Mach 1.92 turbulent jet and its sound field
-
Freund JB Lele SK, Moin P. 2000. Direct numerical simulation of a Mach 1.92 turbulent jet and its sound field. AIAA J. 38(11):2023-31
-
(2000)
AIAA J.
, vol.38
, Issue.11
, pp. 2023-2031
-
-
Freund, J.B.1
Lele, S.K.2
Moin, P.3
-
47
-
-
29244470537
-
The robustness of acoustic analogies
-
AMA Pap. 2005-2940
-
Freund JB, Samanta A, Wei M, Lele SK. 2005. The robustness of acoustic analogies. AMA Pap. 2005-2940
-
(2005)
-
-
Freund, J.B.1
Samanta, A.2
Wei, M.3
Lele, S.K.4
-
48
-
-
36348930574
-
A dynamic subgrid-scale eddy viscosity model
-
Germano M, Piomelli U, Moin P, Cabot WH. 1991. A dynamic subgrid-scale eddy viscosity model. Phys. Fluids A 3(7):1760-65
-
(1991)
Phys. Fluids A
, vol.3
, Issue.7
, pp. 1760-1765
-
-
Germano, M.1
Piomelli, U.2
Moin, P.3
Cabot, W.H.4
-
49
-
-
0041929566
-
Direct computation of the noise radiated by a subsonic cavity flow and application of integral methods
-
Gloerfelt X, Bailly C, Juv́e D. 2 003. Direct computation of the noise radiated by a subsonic cavity flow and application of integral methods. J. Sound Vib. 266(1):119-46
-
(2003)
J. Sound Vib.
, vol.266
, Issue.1
, pp. 119-146
-
-
Gloerfelt, X.1
Bailly, C.2
Juv́e, D.3
-
50
-
-
0016544637
-
The low frequency sound from multipole sources in axisymmetric shear flows, with applications to jet noise
-
Goldstein ME. 1975. The low frequency sound from multipole sources in axisymmetric shear flows, with applications to jet noise. J. Fluid Mech. 70:595-604
-
(1975)
J. Fluid Mech.
, vol.70
, pp. 595-604
-
-
Goldstein, M.E.1
-
51
-
-
0004285993
-
-
New York: McGraw-Hill
-
Goldstein ME. 1976. Aeroacoustia. New York: McGraw-Hill. 293 pp.
-
(1976)
Aeroacoustia
, pp. 293
-
-
Goldstein, M.E.1
-
52
-
-
0021124056
-
Aeroacoustics of turbulent shear flows
-
Goldstein ME. 1984. Aeroacoustics of turbulent shear flows. Anna. Rev. Fluid Mech. 16:263-85
-
(1984)
Anna. Rev. Fluid Mech.
, vol.16
, pp. 263-285
-
-
Goldstein, M.E.1
-
53
-
-
0041856452
-
A generalized acoustic analogy
-
Goldstein ME. 2003. A generalized acoustic analogy. J. Fluid Mech. 488:315-33
-
(2003)
J. Fluid Mech.
, vol.488
, pp. 315-333
-
-
Goldstein, M.E.1
-
54
-
-
14844327761
-
The role of instability waves in predicting jet noise
-
Goldstein ME, Leib SJ. 2005. The role of instability waves in predicting jet noise. J. Flaid Mech. 525:37-72
-
(2005)
J. Flaid Mech.
, vol.525
, pp. 37-72
-
-
Goldstein, M.E.1
Leib, S.J.2
-
55
-
-
0009214918
-
The wall-shear-stress contribution to boundary-layer noise
-
Haj-Hariri H, Akylas TR. 1985. The wall-shear-stress contribution to boundary-layer noise. Phys. Fluids 28(9):2727-29
-
(1985)
Phys. Fluids
, vol.28
, Issue.9
, pp. 2727-2729
-
-
Haj-Hariri, H.1
Akylas, T.R.2
-
56
-
-
0036640671
-
Effects of subgrid scale modeling on time correlations in large eddy simulation
-
He G-W, Rubinstein R, Wang L-P. 2002. Effects of subgrid scale modeling on time correlations in large eddy simulation. Phys. Fluids 14(7):2186-93
-
(2002)
Phys. Fluids
, vol.14
, Issue.7
, pp. 2186-2193
-
-
He, G.-W.1
Rubinstein, R.2
Wang, L.-P.3
-
57
-
-
8844238479
-
On the computation of space-time correlations by large-eddy simulation
-
He G-W, Wang M, Lele SK. 2004. On the computation of space-time correlations by large-eddy simulation. Phys. Fluids 16(11):3859-67
-
(2004)
Phys. Fluids
, vol.16
, Issue.11
, pp. 3859-3867
-
-
He, G.-W.1
Wang, M.2
Lele, S.K.3
-
58
-
-
0038477946
-
Detached-eddy simulations over a simplified landing gear
-
Hedges LS, Travin A, Spalart PR. 2002. Detached-eddy simulations over a simplified landing gear. J. Fluid Eng. 124(2):413-23
-
(2002)
J. Fluid Eng.
, vol.124
, Issue.2
, pp. 413-423
-
-
Hedges, L.S.1
Travin, A.2
Spalart, P.R.3
-
59
-
-
0033241651
-
On the Mach- and Reynolds-number dependence of the flat-plate turbulent boundary layer wall-pressure spectrum
-
Herbert K, Leehey P, Haj-Hariri H. 1999. On the Mach- and Reynolds-number dependence of the flat-plate turbulent boundary layer wall-pressure spectrum. Theor. Compat. Fluid Dyn. 13 (1):33-56
-
(1999)
Theor. Compat. Fluid Dyn.
, vol.13
, Issue.1
, pp. 33-56
-
-
Herbert, K.1
Leehey, P.2
Haj-Hariri, H.3
-
60
-
-
0016558556
-
Contributions to the theory of aerodynamic sound, with application to excess jet noise and the theory of the flute
-
Howe MS. 1975. Contributions to the theory of aerodynamic sound, with application to excess jet noise and the theory of the flute. J. Fluid Mech. 71:625-73
-
(1975)
J. Fluid Mech.
, vol.71
, pp. 625-673
-
-
Howe, M.S.1
-
61
-
-
0018493757
-
The role of surface shear stress fluctuations in the generation of boundary layer noise
-
Howe MS. 1979. The role of surface shear stress fluctuations in the generation of boundary layer noise. J. Sound Vib. 65(2):159-64
-
(1979)
J. Sound Vib.
, vol.65
, Issue.2
, pp. 159-164
-
-
Howe, M.S.1
-
62
-
-
0029144337
-
The damping of sound by wall turbulent shear layers
-
Howe MS. 1995. The damping of sound by wall turbulent shear layers. J. Acoua. Soc. Am. 98(3):1723-30
-
(1995)
J. Acoua. Soc. Am.
, vol.98
, Issue.3
, pp. 1723-1730
-
-
Howe, M.S.1
-
63
-
-
0001440197
-
Trailing edge noise at low Mach numbers
-
Howe MS. 2003. Tbeoq of Vortex Sound. New York: Cambridge Univ. Press. 216 pp
-
Howe MS. 1999. Trailing edge noise at low Mach numbers. J. Sound Vib. 225(2):211-38 Howe MS. 2003. Tbeoq of Vortex Sound. New York: Cambridge Univ. Press. 216 pp.
-
(1999)
J. Sound Vib.
, vol.225
, Issue.2
, pp. 211-238
-
-
Howe, M.S.1
-
64
-
-
0344006664
-
Low-dissipation and low-dispersion Runge-Kutta schemes for computational aeroacoustics
-
Hu FQ, Hussaini MY, Manthey JL. 1996. Low-dissipation and low-dispersion Runge-Kutta schemes for computational aeroacoustics. J. Comp. Pbys. 124(1): 177-91
-
(1996)
J. Comp. Pbys.
, vol.124
, Issue.1
, pp. 177-191
-
-
Hu, F.Q.1
Hussaini, M.Y.2
Manthey, J.L.3
-
65
-
-
0036493462
-
Aeroacoustics of wall-bounded turbulent flows
-
Hu ZW, Morfey CL, Sandham ND. 2002. Aeroacoustics of wall-bounded turbulent flows. AIAA J. 40(3):465-73
-
(2002)
AIAA J.
, vol.40
, Issue.3
, pp. 465-473
-
-
Hu, Z.W.1
Morfey, C.L.2
Sandham, N.D.3
-
67
-
-
0035065963
-
The multiscale formulation of large-eddy simulation: Decay of homogeneous isotropic turbulence
-
Hughes TJR, Mazzei L, Oberai AA, Wray AA. 2001. The multiscale formulation of large-eddy simulation: Decay of homogeneous isotropic turbulence. Phys. Fluids 13(2):505-12
-
(2001)
Phys. Fluids
, vol.13
, Issue.2
, pp. 505-512
-
-
Hughes, T.J.R.1
Mazzei, L.2
Oberai, A.A.3
Wray, A.A.4
-
68
-
-
0034545782
-
Sound generation by coaxial collision of two vortex rings
-
Inoue O, Hattori Y, Sasaki T. 2000. Sound generation by coaxial collision of two vortex rings. J. Fluid Mech. 424:327-65
-
(2000)
J. Fluid Mech.
, vol.424
, pp. 327-365
-
-
Inoue, O.1
Hattori, Y.2
Sasaki, T.3
-
69
-
-
9644264175
-
Modelling of fine-scale turbulence mixing noise
-
Khavaran A, Bridges J. 2005. Modelling of fine-scale turbulence mixing noise. J. Sound Vib. 279(3-5):1131-54
-
(2005)
J. Sound Vib.
, vol.279
, Issue.3-5
, pp. 1131-1154
-
-
Khavaran, A.1
Bridges, J.2
-
71
-
-
0016496982
-
Wave mechanics of boundary layer turbulence and noise
-
Landahl MT. 1975. Wave mechanics of boundary layer turbulence and noise. J. Acoust. Soc. Am. 57(4):824-31
-
(1975)
J. Acoust. Soc. Am.
, vol.57
, Issue.4
, pp. 824-831
-
-
Landahl, M.T.1
-
72
-
-
9144220381
-
Compact finite difference schemes with spectral-like resolution
-
Lele SK. 1992. Compact finite difference schemes with spectral-like resolution. J. Comp. Phys. 103(1):16-42
-
(1992)
J. Comp. Phys.
, vol.103
, Issue.1
, pp. 16-42
-
-
Lele, S.K.1
-
73
-
-
0000470914
-
On sound generated aerodynamically: I. General theory
-
Lighthill MJ. 1952. On sound generated aerodynamically: I. General theory. Proc. R. Soc. London Ser A 211(1107):564-87
-
(1952)
Proc. R. Soc. London Ser A
, vol.211
, Issue.1107
, pp. 564-587
-
-
Lighthill, M.J.1
-
74
-
-
0038650290
-
On the noise from jets
-
AGARD Tech. Rep. CP-131
-
Lilley GM. 1974. On the noise from jets. AGARD Tech. Rep. CP-131
-
(1974)
-
-
Lilley, G.M.1
-
75
-
-
0030084116
-
The radiated noise from isotropic turbulence with applications to the theory of jet noise
-
Lilley GM. 1996. The radiated noise from isotropic turbulence with applications to the theory of jet noise. J. Sound Vib. 190(3):463-76
-
(1996)
J. Sound Vib.
, vol.190
, Issue.3
, pp. 463-476
-
-
Lilley, G.M.1
-
76
-
-
33644601529
-
A proposed modification of the Germano subgrid scale closure method
-
Lilly DK. 1992. A proposed modification of the Germano subgrid scale closure method. Phys. Fluids A 4(3):633-35
-
(1992)
Phys. Fluids A
, vol.4
, Issue.3
, pp. 633-635
-
-
Lilly, D.K.1
-
77
-
-
2942721126
-
Integral acoustic methods: From the (CFD) near-field to the (acoustic) far-field
-
Lyrintzis AS. 2003. Integral acoustic methods: From the (CFD) near-field to the (acoustic) far-field. Int. J. Aeroacoustics 2(2):95-128
-
(2003)
Int. J. Aeroacoustics
, vol.2
, Issue.2
, pp. 95-128
-
-
Lyrintzis, A.S.1
-
78
-
-
85088722313
-
A numerical investigation of sound generation in supersonic jet screech
-
AIAA/CEAS Pap. 2000-2081
-
Manning TA, Lele SK 2000. A numerical investigation of sound generation in supersonic jet screech. AIAA/CEAS Pap. 2000-2081
-
(2000)
-
-
Manning, T.A.1
Lele, S.K.2
-
79
-
-
0033879919
-
Trailing edge noise prediction using large eddy simulation and acoustic analogy
-
Manoha E, Troff B, Sagaut P. 2000. Trailing edge noise prediction using large eddy simulation and acoustic analogy. AIAA J. 38(4):575-83
-
(2000)
AIAA J.
, vol.38
, Issue.4
, pp. 575-583
-
-
Manoha, E.1
Troff, B.2
Sagaut, P.3
-
80
-
-
7244230335
-
Optimal aeroacoustic shape design using the surrogate management framework
-
Marsden AL, Wang M, Dennis JE, Moin P. 2004a. Optimal aeroacoustic shape design using the surrogate management framework. Optim. Eng. 5(2):235-62
-
(2004)
Optim. Eng.
, vol.5
, Issue.2
, pp. 235-262
-
-
Marsden, A.L.1
Wang, M.2
Dennis, J.E.3
Moin, P.4
-
81
-
-
7244224906
-
Suppression of vortex shedding noise via derivative-free shape optimization
-
Marsden AL, Wang M, Dennis JE, Moin P. 2004b. Suppression of vortex shedding noise via derivative-free shape optimization. Phys. Fluids 16(10):L83-86
-
(2004)
Phys. Fluids
, vol.16
, Issue.10
-
-
Marsden, A.L.1
Wang, M.2
Dennis, J.E.3
Moin, P.4
-
82
-
-
33845633524
-
Aerodynamic noise control by optimal shape design
-
Tech. Rep. TF-96, Dep. Mech. Eng., Stanford Univ., Stanford, CA
-
Marsden AL, Wang M, Dennis JE, Moin P. 2005. Aerodynamic noise control by optimal shape design. Tech. Rep. TF-96, Dep. Mech. Eng., Stanford Univ., Stanford, CA
-
(2005)
-
-
Marsden, A.L.1
Wang, M.2
Dennis, J.E.3
Moin, P.4
-
83
-
-
32644445332
-
Direct computation of the sound from a compressible co-rotating vortex pair
-
AIAA Pap. 92-0374
-
Mitchell BE, Lele SK, Moin P. 1992. Direct computation of the sound from a compressible co-rotating vortex pair. AIAA Pap. 92-0374
-
(1992)
-
-
Mitchell, B.E.1
Lele, S.K.2
Moin, P.3
-
84
-
-
0029239953
-
Direct computation of the sound from a compressible co-rotating vortex pair
-
Mitchell BE, Lele SK, Moin P. 1995. Direct computation of the sound from a compressible co-rotating vortex pair. J. Fluid Mech. 285:181-202
-
(1995)
J. Fluid Mech.
, vol.285
, pp. 181-202
-
-
Mitchell, B.E.1
Lele, S.K.2
Moin, P.3
-
85
-
-
0036794746
-
An evaluation of linear instability waves as sources of sound in a supersonic turbulent jet
-
Mohseni Y, Colonius T, Freund JB. 2002. An evaluation of linear instability waves as sources of sound in a supersonic turbulent jet. Phys. Fluids 14(10):3593-600
-
(2002)
Phys. Fluids
, vol.14
, Issue.10
, pp. 3593-3600
-
-
Mohseni, Y.1
Colonius, T.2
Freund, J.B.3
-
86
-
-
0036779266
-
Advances in large-eddy simulation methodology for complex flows
-
Moin P. 2002. Advances in large-eddy simulation methodology for complex flows. Int. J. Heat Fluid Flow 23(5):710-20
-
(2002)
Int. J. Heat Fluid Flow
, vol.23
, Issue.5
, pp. 710-720
-
-
Moin, P.1
-
87
-
-
0000177791
-
A dynamic subgrid-scale model for compressible turbulence and scalar transport
-
Moin P, Squires KD, Cabot VVH, Lee S. 1991. A dynamic subgrid-scale model for compressible turbulence and scalar transport. Phys. Fluids A 3(11):2746-57
-
(1991)
Phys. Fluids A
, vol.3
, Issue.11
, pp. 2746-2757
-
-
Moin, P.1
Squires, K.D.2
Cabot, V.V.H.3
Lee, S.4
-
88
-
-
32644443795
-
The role of viscosity in aerodynamic sound generation
-
Morfey CL. 2003. The role of viscosity in aerodynamic sound generation. Int. J. Aeroacoustics 2(3-4):225-40
-
(2003)
Int. J. Aeroacoustics
, vol.2
, Issue.3-4
, pp. 225-240
-
-
Morfey, C.L.1
-
89
-
-
0034287402
-
Computational procedures for determining structural-acoustic response due to hydrodynamic sources
-
Oberai AA, Roknaldin F, Hughes TJR. 2000. Computational procedures for determining structural-acoustic response due to hydrodynamic sources. Comput. Methods Appl. Mech. Eng. 190(3-4):345-61
-
(2000)
Comput. Methods Appl. Mech. Eng.
, vol.190
, Issue.3-4
, pp. 345-361
-
-
Oberai, A.A.1
Roknaldin, F.2
Hughes, T.J.R.3
-
90
-
-
0036849629
-
Computation of trailing-edge noise due to turbulent flow over an airfoil
-
Oberai AA, Roknaldin F, Hughes TJR. 2002. Computation of trailing-edge noise due to turbulent flow over an airfoil. AIAA J. 40(11):2206-16
-
(2002)
AIAA J.
, vol.40
, Issue.11
, pp. 2206-2216
-
-
Oberai, A.A.1
Roknaldin, F.2
Hughes, T.J.R.3
-
92
-
-
0036435442
-
Wall-layer models for large-eddy simulations
-
Piomelli U, Balaras E. 2002. Wall-layer models for large-eddy simulations. Annu. Rev. Fluid Mech. 34:349-74
-
(2002)
Annu. Rev. Fluid Mech.
, vol.34
, pp. 349-374
-
-
Piomelli, U.1
Balaras, E.2
-
93
-
-
0031248304
-
On the computation of sound by large-eddy simulations
-
Piomelli U, Streett CL, Sarkar S. 1997. On the computation of sound by large-eddy simulations. J. Eng. Math. 32:217-36
-
(1997)
J. Eng. Math.
, vol.32
, pp. 217-236
-
-
Piomelli, U.1
Streett, C.L.2
Sarkar, S.3
-
94
-
-
84953675053
-
Aerodynamic noise and the plane boundary
-
Powell A. 1960. Aerodynamic noise and the plane boundary. J. Acoust. Soc. Am. 32(8):982-90
-
(1960)
J. Acoust. Soc. Am.
, vol.32
, Issue.8
, pp. 982-990
-
-
Powell, A.1
-
95
-
-
84953652461
-
Theory of vortex sound
-
Powell A. 1964. Theory of vortex sound. J. Acoust. Soc. Am. 36(1):177-95
-
(1964)
J. Acoust. Soc. Am.
, vol.36
, Issue.1
, pp. 177-195
-
-
Powell, A.1
-
96
-
-
0000270359
-
Sound propagation in a fluid flowing through an attenuating duct
-
Pridmore-Brown DC. 1958. Sound propagation in a fluid flowing through an attenuating duct. J. Fluid Mech. 9:1-28
-
(1958)
J. Fluid Mech.
, vol.9
, pp. 1-28
-
-
Pridmore-Brown, D.C.1
-
97
-
-
19644372167
-
Numerical simulation of sound radiated from a turbulent vortex ring
-
AIAA Pap. 2004-2918
-
Ran H, Colonius T. 2004. Numerical simulation of sound radiated from a turbulent vortex ring. AIAA Pap. 2004-2918
-
(2004)
-
-
Ran, H.1
Colonius, T.2
-
98
-
-
0014557550
-
Quadrupole correlations governing the pattern of jet noise
-
Ribner HS. 1969. Quadrupole correlations governing the pattern of jet noise. J. Fluid Mech. 38(1):1-24
-
(1969)
J. Fluid Mech.
, vol.38
, Issue.1
, pp. 1-24
-
-
Ribner, H.S.1
-
99
-
-
0034298842
-
Subgrid-scale contribution to noise production in decaying isotropic turbulence
-
Seror C, Sagaut P, Bailly C, Juvé D. 2000. Subgrid-scale contribution to noise production in decaying isotropic turbulence. AIAA J. 38(10):1795-803
-
(2000)
AIAA J.
, vol.38
, Issue.10
, pp. 1795-1803
-
-
Seror, C.1
Sagaut, P.2
Bailly, C.3
Juvé, D.4
-
100
-
-
0035069030
-
On the radiated noise computed by large-eddy simulation
-
Seror C, Sagaut P, Bailly C, Juvé D. 2001. On the radiated noise computed by large-eddy simulation. Phys. Fluids 13(2):476-87
-
(2001)
Phys. Fluids
, vol.13
, Issue.2
, pp. 476-487
-
-
Seror, C.1
Sagaut, P.2
Bailly, C.3
Juvé, D.4
-
101
-
-
32644451305
-
A numerical experiment to determine whether surface shear-stress fluctuations are a true sound source
-
In press
-
Shariff K, Wang M. 2005. A numerical experiment to determine whether surface shear-stress fluctuations are a true sound source. Phys. Fluids. In press
-
(2005)
Phys. Fluids
-
-
Shariff, K.1
Wang, M.2
-
102
-
-
0034188604
-
Effects of jet temperature and nozzle-lip thickness on screech tones
-
Shen H, Tam CKW. 2000. Effects of jet temperature and nozzle-lip thickness on screech tones. AIAA J. 38(5):762-67
-
(2000)
AIAA J.
, vol.38
, Issue.5
, pp. 762-767
-
-
Shen, H.1
Tam, C.K.W.2
-
103
-
-
0036151748
-
Three-dimensional numerical simulation of the jet screech phenomenon
-
Shen H, Tam CKW. 2002. Three-dimensional numerical simulation of the jet screech phenomenon. AIAA J. 40(1):33-41
-
(2002)
AIAA J.
, vol.40
, Issue.1
, pp. 33-41
-
-
Shen, H.1
Tam, C.K.W.2
-
104
-
-
29244438385
-
Noise prediction for increasingly complex jets. Part I: Methods and tests
-
Shur ML, Spalart PR, Strelets MKh. 2005a. Noise prediction for increasingly complex jets. Part I: methods and tests. Int. J. Aeroacoustics. 4:213-46
-
(2005)
Int. J. Aeroacoustics.
, vol.4
, pp. 213-246
-
-
Shur, M.L.1
Spalart, P.R.2
Strelets, M.Kh.3
-
105
-
-
29244438385
-
Noise prediction for increasingly complex jets. Part II: Applications
-
Shur ML, Spalart PR, Strelets MKh. 2005b. Noise prediction for increasingly complex jets. Part II: applications. Int. J. Aeroacoustics. 4:247-66
-
(2005)
Int. J. Aeroacoustics.
, vol.4
, pp. 247-266
-
-
Shur, M.L.1
Spalart, P.R.2
Strelets, M.Kh.3
-
106
-
-
0033752513
-
Simulation of acoustic scattering from a trailing edge
-
Singer BA, Brentner KS, Lockard DP, Lilley GM. 2000. Simulation of acoustic scattering from a trailing edge. J. Sound Vib. 230(3):541-60
-
(2000)
J. Sound Vib.
, vol.230
, Issue.3
, pp. 541-560
-
-
Singer, B.A.1
Brentner, K.S.2
Lockard, D.P.3
Lilley, G.M.4
-
107
-
-
3142755155
-
Development of computational aeroacoustics tools for airframe noise calculations
-
Singer BA, Guo Y. 2004. Development of computational aeroacoustics tools for airframe noise calculations. Int. J. Comput. Fluid Dyn. 18(6):455-69
-
(2004)
Int. J. Comput. Fluid Dyn.
, vol.18
, Issue.6
, pp. 455-469
-
-
Singer, B.A.1
Guo, Y.2
-
108
-
-
0001957739
-
General circulation experiments with the primitive equations. I. The basic experiment
-
Smagorinsky J. 1963. General circulation experiments with the primitive equations. I. The basic experiment. Mon. Weather Rev. 91:99-164
-
(1963)
Mon. Weather Rev.
, vol.91
, pp. 99-164
-
-
Smagorinsky, J.1
-
109
-
-
0002054570
-
Comments on the feasibility of LES for wings and a hybrid RANS/LES approach
-
ed. C Liu, Z Liu, L Sakell, Columbus, OH: Greyden. 676 pp
-
Spalart PR, Jou VVH, Strelets M, Allmaras SR. 1997. Comments on the feasibility of LES for wings and a hybrid RANS/LES approach. In Advances in DNS/LES. Proc. 1st AFOSR Int. Conf. DNS/LES, ed. C Liu, Z Liu, L Sakell, pp. 137-47. Columbus, OH: Greyden. 676 pp.
-
(1997)
Advances in DNS/LES. Proc. 1st AFOSR Int. Conf. DNS/LES
, pp. 137-147
-
-
Spalart, P.R.1
Jou, V.V.H.2
Strelets, M.3
Allmaras, S.R.4
-
110
-
-
0013086767
-
An approximate deconvolution procedure for large-eddy simulation
-
Stolz S, Adams NA. 1999. An approximate deconvolution procedure for large-eddy simulation. Phys. Fluids 11(7):1699-701
-
(1999)
Phys. Fluids
, vol.11
, Issue.7
, pp. 1699-1701
-
-
Stolz, S.1
Adams, N.A.2
-
111
-
-
0018936164
-
Flow field and acoustic properties of a Mach number 0.9 jet at a low Reynolds number
-
Stromberg JL, McLaughlin DK, Troutt TR. 1980. Flow field and acoustic properties of a Mach number 0.9 jet at a low Reynolds number. J. Sound Kh. 72(2):159-76
-
(1980)
J. Sound Kh.
, vol.72
, Issue.2
, pp. 159-176
-
-
Stromberg, J.L.1
McLaughlin, D.K.2
Troutt, T.R.3
-
112
-
-
0141787982
-
Shock leakage through an unsteady vortex-laden mixing layer: Application to jet screech
-
Suzuki T, Lele SK 2003. Shock leakage through an unsteady vortex-laden mixing layer: application to jet screech. J. Fluid Mech. 490:139-67
-
(2003)
J. Fluid Mech.
, vol.490
, pp. 139-167
-
-
Suzuki, T.1
Lele, S.K.2
-
113
-
-
3142724329
-
Computational aeroacoustics: An overview of computational challenges and applications
-
Tam CKW. 2004. Computational aeroacoustics: an overview of computational challenges and applications. Int. J. Comput. Fluid Dyn. 18(6):547-67
-
(2004)
Int. J. Comput. Fluid Dyn.
, vol.18
, Issue.6
, pp. 547-567
-
-
Tam, C.K.W.1
-
114
-
-
0033078892
-
Jet mixing noise from fine-scale turbulence
-
Tam CKW, Auriault L. 1999. Jet mixing noise from fine-scale turbulence. AIAA J. 37(2):145-53
-
(1999)
AIAA J.
, vol.37
, Issue.2
, pp. 145-153
-
-
Tam, C.K.W.1
Auriault, L.2
-
115
-
-
19644369292
-
Dispersion-relation-preserving finite difference schemes for computational acoustics
-
Tam CKW, Webb JC. 1993. Dispersion-relation-preserving finite difference schemes for computational acoustics. J. Comp. Phys. 107(2):262-81
-
(1993)
J. Comp. Phys.
, vol.107
, Issue.2
, pp. 262-281
-
-
Tam, C.K.W.1
Webb, J.C.2
-
116
-
-
0017769562
-
An experimental study of jet noise. Part I: Turbulent mixing noise
-
Tanna HK 1977. An experimental study of jet noise. Part I: Turbulent mixing noise. J. Sound Vib. 50(3):405-28
-
(1977)
J. Sound Vib.
, vol.50
, Issue.3
, pp. 405-428
-
-
Tanna, H.K.1
-
117
-
-
0033715429
-
Detached-eddy simulations past a circular cylinder
-
Travin A, Shur M, Strelets M, Spalart P. 2000. Detached-eddy simulations past a circular cylinder. Flow Turb. Combust. 63 (1-4):293-313
-
(2000)
Flow Turb. Combust.
, vol.63
, Issue.1-4
, pp. 293-313
-
-
Travin, A.1
Shur, M.2
Strelets, M.3
Spalart, P.4
-
118
-
-
32644434672
-
Computational prediction of flow generated sound
-
Cent. Turbul. Res., Stanford Univ./NASA Ames, Stanford, CA
-
Wang M, Freund JB, Lele SK 2005. Computational prediction of flow generated sound. CTR Manuscript 190, Cent. Turbul. Res., Stanford Univ./ NASA Ames, Stanford, CA
-
(2005)
CTR Manuscript 190
-
-
Wang, M.1
Freund, J.B.2
Lele, S.K.3
-
119
-
-
0001054469
-
Computation of quadrupole noise using acoustic analogy
-
Wang M, Lele SY, Moin P. 1996a. Computation of quadrupole noise using acoustic analogy. AIAA J. 34(11):2247-54
-
(1996)
AIAA J.
, vol.34
, Issue.11
, pp. 2247-2254
-
-
Wang, M.1
Lele, S.Y.2
Moin, P.3
-
120
-
-
0030184099
-
Sound radiation during local laminar breakdown in a low Mach number boundary layer
-
Wang M, Lele SY, Moin P. 1996b. Sound radiation during local laminar breakdown in a low Mach number boundary layer. J. Fluid Mech. 319:197-218
-
(1996)
J. Fluid Mech.
, vol.319
, pp. 197-218
-
-
Wang, M.1
Lele, S.Y.2
Moin, P.3
-
121
-
-
0034504239
-
Computation of trailing-edge flow and noise using large-eddy simulation
-
Wang M, Moin P. 2000. Computation of trailing-edge flow and noise using large-eddy simulation. AIAA J. 38(12):2201-9
-
(2000)
AIAA J.
, vol.38
, Issue.12
, pp. 2201-2209
-
-
Wang, M.1
Moin, P.2
-
122
-
-
0036640410
-
Dynamic wall modeling for large-eddy simulation of complex turbulent flows
-
Wang M, Moin P. 2002. Dynamic wall modeling for large-eddy simulation of complex turbulent flows. Phys. Fluids 14(7):2043-51
-
(2002)
Phys. Fluids
, vol.14
, Issue.7
, pp. 2043-2051
-
-
Wang, M.1
Moin, P.2
-
123
-
-
29244486747
-
LES prediction of pressure fluctuations on a low-speed airfoil
-
Cent. Turbul. Res., Stanford Univ./NASA Ames, Stanford, CA
-
Wang M, Moreau S, Iaccarino G, Roger M. 2004. LES prediction of pressure fluctuations on a low-speed airfoil. Annu. Res. Briefs, Cent. Turbul. Res., Stanford Univ./NASA Ames, Stanford, CA, pp. 183-93
-
(2004)
Annu. Res. Briefs
, pp. 183-193
-
-
Wang, M.1
Moreau, S.2
Iaccarino, G.3
Roger, M.4
-
124
-
-
29244489490
-
A noise-controlled free shear flow
-
In press
-
Wei M, Freund JB. 2005. A noise-controlled free shear flow. J. Fluid Mech. In press
-
(2005)
J. Fluid Mech.
-
-
Wei, M.1
Freund, J.B.2
-
125
-
-
0000314584
-
Computing aerodynamically generated noise
-
Wells VL, Renaut RA. 1997. Computing aerodynamically generated noise. Annu. Rev. Fluid Mech. 29:161-99
-
(1997)
Annu. Rev. Fluid Mech.
, vol.29
, pp. 161-199
-
-
Wells, V.L.1
Renaut, R.A.2
|