01319nam a2200361 i 450099100146174970753620020507193901.0931106s1988 uk ||| | eng 0521358833b10850727-39ule_instLE01312605ExLDip.to Matematicaeng531AMS 70-01AMS 70-XXAMS 70DAMS 70EAMS 70FWhittaker, E. T.123012A treatise on the analytical dynamics of particles and rigid bodies :with an introduction to the problem of three bodies /E. T. Witthaker4th ed., with forewordCambridge :Cambridge University Press,1988xvii, 456 p. ;23 cm.Cambridge mathematical libraryDynamics of a particleDynamics of rigid bodiesMechanics of particles and systems.b1085072723-02-1728-06-02991001461749707536LE013 70-XX WHI11 (1988)12013000120430le013-E0.00-l- 041840.i1096196328-06-02Treatise on the analytical dynamics of particles and rigid bodies107260UNISALENTOle01301-01-93ma -enguk 2101849nam 2200505I 450 991070525140332120141212144352.0(CKB)5470000002448853(OCoLC)898080688(EXLCZ)99547000000244885320141212j201306 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierLarge Civil Tiltrotor (LCTR2) interior noise predictions due to turbulent boundary layer excitation /Ferdinand W. GrosveldHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,June 2013.1 online resource (37 pages) color illustrationsNASA-CR ;2013-218005Title from title screen (viewed Dec. 12, 2014)."June 2013."Includes bibliographical references (pages 17-18).Large Civil Tiltrotor Acoustic propertiesnasatFinite element methodnasatTurbulent boundary layernasatTilt rotor aircraftnasatSound pressurenasatFrequency responsenasatAcoustic properties.Finite element method.Turbulent boundary layer.Tilt rotor aircraft.Sound pressure.Frequency response.Grosveld Ferdinand W.1391334Langley Research Center,United States.National Aeronautics and Space Administration,GPOGPOBOOK9910705251403321Large Civil Tiltrotor (LCTR2) interior noise predictions due to turbulent boundary layer excitation3539259UNINA