메뉴 건너뛰기




Volumn , Issue , 2004, Pages 8780-8792

Experimental and computational evaluation of flush-mounted, S-duct inlets

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; BOUNDARY LAYERS; CRYOGENIC LIQUIDS; DRAG; DUCTS; INTAKE SYSTEMS; NAVIER STOKES EQUATIONS; REYNOLDS NUMBER; TRANSONIC AERODYNAMICS; TRANSONIC FLOW;

EID: 2942702188     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-764     Document Type: Conference Paper
Times cited : (63)

References (22)
  • 1
    • 0027264322 scopus 로고
    • Wake ingestion propulsion benefit
    • Jan.-Feb.
    • Smith, Leroy H.: Wake Ingestion Propulsion Benefit. Journal of Aircraft and Power, Vol. 9, No. 1, Jan.-Feb., 1993.
    • (1993) Journal of Aircraft and Power , vol.9 , Issue.1
    • Smith, L.H.1
  • 2
    • 34250886077 scopus 로고
    • Design and testing of new center inlet and S-Duct for B-727 airplane with refanned JT8D engines
    • Jan.
    • Ting, C.T.; Kaldschmidt, G.; and Syltebo, B.E.: Design and Testing of New Center Inlet and S-Duct for B-727 Airplane With Refanned JT8D Engines. AIAA Paper 75-0059, Jan., 1975.
    • (1975) AIAA Paper , vol.75 , Issue.59
    • Ting, C.T.1    Kaldschmidt, G.2    Syltebo, B.E.3
  • 11
    • 84913574655 scopus 로고
    • Calibration of the 13- by 13-Inch adaptive wall test section for the langley 0.3-Meter transonic cryogenic tunnel
    • Dec.
    • Mineck, Raymond E.; and Hill, Acquilla S.: Calibration of the 13- by 13-Inch Adaptive Wall Test Section for the Langley 0.3-Meter Transonic Cryogenic Tunnel. NASA Technical Paper 3049, Dec. 1990.
    • (1990) NASA Technical Paper , vol.3049
    • Mineck, R.E.1    Hill, A.S.2
  • 12
    • 0012361899 scopus 로고
    • Operating envelope charts for the langley 0.3-Meter transonic cryogenic wind tunnel
    • Aug.
    • Rallo, Rosemary A.; Dress, David A.; and Siegle, Henry J.A.: Operating Envelope Charts for the Langley 0.3-Meter Transonic Cryogenic Wind Tunnel. NASA Technical Memorandum 89008, Aug. 1986.
    • (1986) NASA Technical Memorandum 89008
    • Rallo, R.A.1    Dress, D.A.2    Siegle, H.J.A.3
  • 13
    • 28844467530 scopus 로고
    • Gas turbine engine inlet flow distortion
    • March
    • Anon.: Gas Turbine Engine Inlet Flow Distortion. Society of Automotive Engineers Report ARP-1420, March 1978.
    • (1978) Society of Automotive Engineers Report , vol.ARP-1420
  • 16
    • 0003471396 scopus 로고
    • Improved two-equation turbulence model for aerodynamic flow
    • Menter, F.: Improved Two-Equation Turbulence Model for Aerodynamic Flow. NASA Technical Memorandum 103975, 1992.
    • (1992) NASA Technical Memorandum 103975
    • Menter, F.1
  • 19
    • 0003631917 scopus 로고    scopus 로고
    • Aircraft design: A conceptual approach. Third Edition
    • American Institute of Aeronautics and Astronautics, Inc.
    • Raymer, Daniel P.: Aircraft Design: A Conceptual Approach. Third Edition. AIAA Education Series. American Institute of Aeronautics and Astronautics, Inc., 1999.
    • (1999) AIAA Education Series
    • Raymer, D.P.1
  • 22
    • 34250837834 scopus 로고    scopus 로고
    • Evaluation of flush-mounted, s-duct inlets with large amounts of boundary layer ingestion
    • Warsaw, Poland. Paper No. 38, October 6-9
    • Berrier, Bobby L.; and Morehouse, Melissa B.: Evaluation of Flush-Mounted, S-Duct Inlets With Large Amounts of Boundary Layer Ingestion. Research and Technology Agency Symposium on Vehicle Propulsion Integration. Warsaw, Poland. Paper No. 38, October 6-9, 2003.
    • (2003) Research and Technology Agency Symposium on Vehicle Propulsion Integration
    • Berrier, B.L.1    Morehouse, M.B.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.