메뉴 건너뛰기




Volumn , Issue , 2009, Pages

Supersonic jet noise from a conical C-D nozzle with forward flight effects

Author keywords

[No Author keywords available]

Indexed keywords

C-D NOZZLE; CONVERGENT-DIVERGENT NOZZLE; FAR-FIELD; FAR-FIELD NOISE; FORWARD FLIGHT; KIRCHHOFF INTEGRAL; NOZZLE THROAT; SCREECH TONES; SHOCK NOISE; SHOCK-CELL; SUPERSONIC JETS;

EID: 78549290670     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (11)

References (13)
  • 2
    • 0032687201 scopus 로고    scopus 로고
    • Effects of counterflow on the aeroacoustic properties of a supersont jet
    • Shih, F. S., Alvi, D.M. (1999). Effects of Counterflow on the Aeroacoustic Properties of a Supersont Jet. Journal of Aircraft, 36:451-457.
    • (1999) Journal of Aircraft , vol.36 , pp. 451-457
    • Shih, F.S.1    Alvi, D.M.2
  • 3
    • 0034793098 scopus 로고    scopus 로고
    • On the sound sources of screech tones radiated from choked circular jets
    • Umeda, Y., and Ishii, R. (2001). "On the sound sources of screech tones radiated from choked circular jets" J. Acoust. Soc. Am, 110:1845-1858.
    • (2001) J. Acoust. Soc. Am , vol.110 , pp. 1845-1858
    • Umeda, Y.1    Ishii, R.2
  • 5
    • 0021494887 scopus 로고
    • Acoustic near-field properties associated with broadband shock noise
    • Seiner, J.M., Yu, J.C. (1984). "Acoustic near-field properties associated with broadband shock noise" AIAA Journal, 22:1207-1215.
    • (1984) AIAA Journal , vol.22 , pp. 1207-1215
    • Seiner, J.M.1    Yu, J.C.2
  • 7
    • 10944258281 scopus 로고
    • Development and validation of highly modular flow solver versions in g2dflow and g3dflow
    • Sweden
    • Eriksson, L.-E. 1995 Development and validation of highly modular flow solver versions in g2dflow and g3dflow. Internal report 9970-1162. Volvo Aero Corporation, Sweden.
    • (1995) Internal Report 9970-1162. Volvo Aero Corporation
    • Eriksson, L.-E.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.