UNIFIED APPROACH TO AERODYNAMIC SOUND GENERATION IN PRESENCE OF SOLID BOUNDARIES

[1] CROW SC, 1970, STUDIES APPLIED MATH, V49

[2] THE INFLUENCE OF SOLID BOUNDARIES UPON AERODYNAMIC SOUND [J]. PROCEEDINGS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL AND PHYSICAL SCIENCES, 1955, 231 (1187): : 505 - 514

[3] DOAK PE, 1960, P ROY SOC LOND A MAT, V259, P129

[4] Ffowcs-Williams J. E., 1969, J SOUND VIB, V10, P10

[5] FFOWCSWILLIAMS JE, 1970, J FLUID MECH, V40, P657

[6] FFOWCSWILLIAMS JE, 1969, T R SOC LOND A, V264, P321

[7] GOLDSTEIN M, 1974, D7680 NASA TN

[8] Gutin L., 1948, 1195 NACA

[9] HAWKINGS DL, 1973, P BRIT ACOUST SOC, V2

[10] LANSING DL, 1970, SP228 NASA, P323

[1] CROW SC, 1970, STUDIES APPLIED MATH, V49

[2] THE INFLUENCE OF SOLID BOUNDARIES UPON AERODYNAMIC SOUND [J]. PROCEEDINGS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL AND PHYSICAL SCIENCES, 1955, 231 (1187): : 505 - 514

[3] DOAK PE, 1960, P ROY SOC LOND A MAT, V259, P129

[4] Ffowcs-Williams J. E., 1969, J SOUND VIB, V10, P10

[5] FFOWCSWILLIAMS JE, 1970, J FLUID MECH, V40, P657

[6] FFOWCSWILLIAMS JE, 1969, T R SOC LOND A, V264, P321

[7] GOLDSTEIN M, 1974, D7680 NASA TN

[8] Gutin L., 1948, 1195 NACA

[9] HAWKINGS DL, 1973, P BRIT ACOUST SOC, V2

[10] LANSING DL, 1970, SP228 NASA, P323