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Volumn 208, Issue 5, 1997, Pages 803-822

The aeroacoustics and aerodynamics of high-speed Coanda devices, part 2: Effects of modifications for flow control and noise reduction

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC NOISE; AERODYNAMICS; BODIES OF REVOLUTION; FLOW CONTROL; JETS; MEASUREMENTS; NOISE ABATEMENT; NOZZLES; SUPERSONIC FLOW; VISUALIZATION;

EID: 0031334129     PISSN: 0022460X     EISSN: None     Source Type: Journal    
DOI: 10.1006/jsvi.1997.1203     Document Type: Article
Times cited : (22)

References (26)
  • 1
    • 0031354648 scopus 로고    scopus 로고
    • The aeroacoustics and aerodynamics of high-speed Coanda devices, Part 1: Conventional arrangement of exit nozzle and surface
    • P. W. CARPENTER and P. N. GREEN 1997 Journal of Sound and Vibration 208, 777-801. The aeroacoustics and aerodynamics of high-speed Coanda devices, Part 1: conventional arrangement of exit nozzle and surface.
    • (1997) Journal of Sound and Vibration , vol.208 , pp. 777-801
    • Carpenter, P.W.1    Green, P.N.2
  • 8
    • 0141981634 scopus 로고
    • An analysis of base pressure at supersonic velocities and comparison with experiments
    • D. R. CHAPMAN 1950 NACA Technical Note 2137. An analysis of base pressure at supersonic velocities and comparison with experiments.
    • (1950) NACA Technical Note 2137
    • Chapman, D.R.1
  • 9
    • 85143761046 scopus 로고
    • A theory for base pressures in transonic and supersonic flow
    • H. H. KORST 1956 Journal of Applied Mechanics 23, 593-600. A theory for base pressures in transonic and supersonic flow.
    • (1956) Journal of Applied Mechanics , vol.23 , pp. 593-600
    • Korst, H.H.1
  • 10
    • 0028486591 scopus 로고
    • The effects of base steps and axisymmetry on supersonic jets over Coanda surfaces
    • D. G. GREGORY-SMITH and P. SENIOR 1994 International Journal of Heat and Fluid Flow 15, 291-298. The effects of base steps and axisymmetry on supersonic jets over Coanda surfaces.
    • (1994) International Journal of Heat and Fluid Flow , vol.15 , pp. 291-298
    • Gregory-Smith, D.G.1    Senior, P.2
  • 12
    • 0001254490 scopus 로고
    • On the noise emanating from a two-dimensional jet above the critical pressure
    • A. POWELL 1953 Aeronautical Quarterly 4, 103-122. On the noise emanating from a two-dimensional jet above the critical pressure.
    • (1953) Aeronautical Quarterly , vol.4 , pp. 103-122
    • Powell, A.1
  • 13
    • 0003330719 scopus 로고
    • Wind tunnel experiments in the flow over rectangular cavities at subsonic and transonic speeds
    • J. E. ROSSITER 1966 Aeronautical Research Council, R & M 3438. Wind tunnel experiments in the flow over rectangular cavities at subsonic and transonic speeds.
    • (1966) Aeronautical Research Council, R & M , vol.3438
    • Rossiter, J.E.1
  • 17
    • 0024138186 scopus 로고
    • The compressible turbulent shear layer: An experimental study
    • D. PAPAMOSCHOU and A. ROSHKO 1988 Journal of Fluid Mechanics 197, 453-477. The compressible turbulent shear layer: an experimental study.
    • (1988) Journal of Fluid Mechanics , vol.197 , pp. 453-477
    • Papamoschou, D.1    Roshko, A.2
  • 21
    • 0017769564 scopus 로고
    • An experimental study of jet noise, part II: Shock associated noise
    • H. K. TANNA 1977 Journal of Sound and Vibration 50, 429-444. An experimental study of jet noise, part II: shock associated noise.
    • (1977) Journal of Sound and Vibration , vol.50 , pp. 429-444
    • Tanna, H.K.1
  • 25
    • 0000991011 scopus 로고
    • Control of an axisymmetric jet using vortex generators
    • K. B. M. Q. ZAMAN, M. F. REEDER and M. SAMIMY 1994 Physics of Fluids 6, 778-793. Control of an axisymmetric jet using vortex generators.
    • (1994) Physics of Fluids , vol.6 , pp. 778-793
    • Zaman, K.B.M.Q.1    Reeder, M.F.2    Samimy, M.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.