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Volumn , Issue , 1999, Pages 1022-1033

Measurement of reynolds number effect on airframe noise in the 12-foot pressure wind tunnel

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC GENERATORS; ACOUSTIC NOISE MEASUREMENT; AEROACOUSTICS; AIRFRAMES; LIFT; NASA; REYNOLDS NUMBER; STRUCTURAL FRAMES; WIND TUNNELS;

EID: 84983189297     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1999-1959     Document Type: Conference Paper
Times cited : (18)

References (20)
  • 3
    • 0017525574 scopus 로고
    • Sound Radiation from Aircraft Wheel-Well/Landing-Gear Configurations
    • Heller, H., Dobrzynski, W. “Sound Radiation from Aircraft Wheel-Well/Landing-Gear Configurations,” Journal of Aircraft, vol. 14, no. 8, 768-774, 1977.
    • (1977) Journal of Aircraft , vol.14 , Issue.8 , pp. 768-774
    • Heller, H.1    Dobrzynski, W.2
  • 6
    • 84896840842 scopus 로고    scopus 로고
    • Array Design for Non-intrusive Measurements of Noise Sources
    • Underbrink, J., Dougherty, R. “Array Design for Non-intrusive Measurements of Noise Sources,” NOISECON 96, 1996. 7
    • (1996) NOISECON , vol.96 , pp. 7
    • Underbrink, J.1    Dougherty, R.2
  • 12
    • 0019020766 scopus 로고
    • Noise Radiation from the Side Edges of Flaps
    • May
    • Hardin, J. C. “Noise Radiation from the Side Edges of Flaps,” AIAA J., vol. 18, no. 5, May 1980, 549-552.
    • (1980) AIAA J , vol.18 , Issue.5 , pp. 549-552
    • Hardin, J.C.1
  • 16
    • 84977103645 scopus 로고    scopus 로고
    • 4lh AIAA/CEAS Aeroacoutics Conference, AIAA-98-2226, Toulouse, France, June
    • Streett, C. “Numerical Simulation of a Flap-edge Flowfield,” 4lh AIAA/CEAS Aeroacoutics Conference, AIAA-98-2226, Toulouse, France, June 1998.
    • (1998) Numerical Simulation of a Flap-Edge Flowfield
    • Streett, C.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.