These tools will no longer be maintained as of December 31, 2024. Archived website can be found here. PubMed4Hh GitHub repository can be found here. Contact NLM Customer Service if you have questions.


Pubmed for Handhelds

PUBMED FOR HANDHELDS

Journal Abstract Search

153 related items for PubMed ID: 21476623

  • 1. On the aeroacoustic tonal noise generation mechanism of a sharp-edged plate.
    Moreau DJ, Brooks LA, Doolan CJ.
    J Acoust Soc Am; 2011 Apr; 129(4):EL154-60. PubMed ID: 21476623
    [Abstract] [Full Text] [Related]

  • 2. Broadband trailing edge noise from a sharp-edged strut.
    Moreau DJ, Brooks LA, Doolan CJ.
    J Acoust Soc Am; 2011 May; 129(5):2820-9. PubMed ID: 21568386
    [Abstract] [Full Text] [Related]

  • 3. Covariance-based approaches to aeroacoustic noise source analysis.
    Du L, Xu L, Li J, Guo B, Stoica P, Bahr C, Cattafesta LN.
    J Acoust Soc Am; 2010 Nov; 128(5):2877-87. PubMed ID: 21110583
    [Abstract] [Full Text] [Related]

  • 4. Symmetric airfoil geometry effects on leading edge noise.
    Gill J, Zhang X, Joseph P.
    J Acoust Soc Am; 2013 Oct; 134(4):2669-80. PubMed ID: 24116405
    [Abstract] [Full Text] [Related]

  • 5. Acoustic intensity-based method for sound radiations in a uniform flow.
    Yu C, Zhou Z, Zhuang M.
    J Acoust Soc Am; 2009 Nov; 126(5):2198-205. PubMed ID: 19894800
    [Abstract] [Full Text] [Related]

  • 6. Limits of coherence-based aeroacoustic analysis in the presence of distributed sources.
    Bahr C, Cattafesta LN.
    J Acoust Soc Am; 2011 Jun; 129(6):EL248-53. PubMed ID: 21682360
    [Abstract] [Full Text] [Related]

  • 7. Aeroacoustic sound generation in simple expansion chambers.
    English EJ, Holland KR.
    J Acoust Soc Am; 2010 Nov; 128(5):2589-95. PubMed ID: 21110557
    [Abstract] [Full Text] [Related]

  • 8. Point vortex model for prediction of sound generated by a wing with flap interacting with a passing vortex.
    Manela A, Huang L.
    J Acoust Soc Am; 2013 Apr; 133(4):1934-44. PubMed ID: 23556563
    [Abstract] [Full Text] [Related]

  • 9. A computational study of the effect of windscreen shape and flow resistivity on turbulent wind noise reduction.
    Xu Y, Zheng ZC, Wilson DK.
    J Acoust Soc Am; 2011 Apr; 129(4):1740-7. PubMed ID: 21476631
    [Abstract] [Full Text] [Related]

  • 10. A synthesis approach for reproducing the response of aircraft panels to a turbulent boundary layer excitation.
    Bravo T, Maury C.
    J Acoust Soc Am; 2011 Jan; 129(1):143-53. PubMed ID: 21302997
    [Abstract] [Full Text] [Related]

  • 11. "Ladder" structure in tonal noise generated by laminar flow around an airfoil.
    Chong TP, Joseph P.
    J Acoust Soc Am; 2012 Jun; 131(6):EL461-7. PubMed ID: 22713022
    [Abstract] [Full Text] [Related]

  • 12. The effect of acoustic forcing on an airfoil tonal noise mechanism.
    Schumacher KL, Doolan CJ, Kelso RM.
    J Acoust Soc Am; 2014 Aug; 136(2):EL78-83. PubMed ID: 25096150
    [Abstract] [Full Text] [Related]

  • 13. Effect of trailing-edge serrations on noise reduction in a coupled bionic aerofoil inspired by barn owls.
    Li D, Liu X, Hu F, Wang L.
    Bioinspir Biomim; 2019 Dec 04; 15(1):016009. PubMed ID: 31665715
    [Abstract] [Full Text] [Related]

  • 14. Near-field vector intensity measurements of a small solid rocket motor.
    Gee KL, Giraud JH, Blotter JD, Sommerfeldt SD.
    J Acoust Soc Am; 2010 Aug 04; 128(2):EL69-74. PubMed ID: 20707417
    [Abstract] [Full Text] [Related]

  • 15. Investigation of higher spanwise Helmholtz resonance modes in slender covered cavities.
    de Jong AT, Bijl H.
    J Acoust Soc Am; 2010 Oct 04; 128(4):1668-78. PubMed ID: 20968339
    [Abstract] [Full Text] [Related]

  • 16. On the manipulation of flow and acoustic fields of a blunt trailing edge aerofoil by serrated leading edges.
    Hasheminejad SM, Chong TP, Lacagnina G, Joseph P, Kim JH, Choi KS, Omidyeganeh M, Pinelli A, Stalnov O.
    J Acoust Soc Am; 2020 Jun 04; 147(6):3932. PubMed ID: 32611165
    [Abstract] [Full Text] [Related]

  • 17. The role of nonlinear effects in the propagation of noise from high-power jet aircraft.
    Gee KL, Sparrow VW, James MM, Downing JM, Hobbs CM, Gabrielson TB, Atchley AA.
    J Acoust Soc Am; 2008 Jun 04; 123(6):4082-93. PubMed ID: 18537360
    [Abstract] [Full Text] [Related]

  • 18. Tailored nearfield Green's functions for arbitrary geometries.
    Bonamy C, Jordan P, Gervais Y.
    J Acoust Soc Am; 2010 Nov 04; 128(5):2581-8. PubMed ID: 21110556
    [Abstract] [Full Text] [Related]

  • 19. Measurement of wind noise levels in streamlined probes.
    Webster J, Raspet R, Yu J, Prather WE.
    J Acoust Soc Am; 2010 May 04; 127(5):2764-70. PubMed ID: 21117725
    [Abstract] [Full Text] [Related]

  • 20. A multi-mode screech frequency prediction formula for circular supersonic jets.
    Gao JH, Li XD.
    J Acoust Soc Am; 2010 Mar 04; 127(3):1251-7. PubMed ID: 20329824
    [Abstract] [Full Text] [Related]

    Page: [Next] [New Search]
    of 8.