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Volumn , Issue , 1998, Pages

Validation of an automated chimera methodology for aircraft escape systems analysis

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AUTOMATION; COMPUTATIONAL FLUID DYNAMICS; DEGREES OF FREEDOM (MECHANICS); DOMAIN DECOMPOSITION METHODS; EJECTION SEATS; SAFETY TESTING; SUPERSONIC AIRCRAFT; SYSTEMS ANALYSIS;

EID: 84982318316     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-767     Document Type: Conference Paper
Times cited : (16)

References (15)
  • 1
    • 84983126875 scopus 로고    scopus 로고
    • Computational Fluid Dynamics Tools for Escape Systems Aerodynamic Analysis
    • CFDRC Report #4128/17, December
    • Habchi, S.D., Rock, S.G., Hufford, G.S., Parthasarthy, V.J., and Przekwas, A.J., "Computational Fluid Dynamics Tools for Escape Systems Aerodynamic Analysis," Final Report, CFDRC Report #4128/17, December 1996.
    • (1996) Final Report
    • Habchi, S.D.1    Rock, S.G.2    Hufford, G.S.3    Parthasarthy, V.J.4    Przekwas, A.J.5
  • 2
    • 85072461289 scopus 로고
    • CFD Analysis of Ejection Seat Escape Systems
    • Aerotech '92, Anaheim, CA
    • Habchi, S.D., Przekwas, A J., Marquette, T. and Ayoub, P., "CFD Analysis of Ejection Seat Escape Systems," SAE 921924\ Aerotech '92, Anaheim, CA, 1992.
    • (1992) SAE 921924
    • Habchi, S.D.1    Przekwas, A.J.2    Marquette, T.3    Ayoub, P.4
  • 3
    • 84873861919 scopus 로고
    • Computational Aerodynamic Analysis of the Navy Aircrew Common Ejection Seat
    • January
    • Habchi, S.D., Ho, S.Y., Hufford, G.S., Marquette, T., and Ayoub. P., "Computational Aerodynamic Analysis of the Navy Aircrew Common Ejection Seat," AIAA-94-0395, January 1994.
    • (1994) AIAA-94-0395
    • Habchi, S.D.1    Ho, S.Y.2    Hufford, G.S.3    Marquette, T.4    Ayoub, P.5
  • 4
    • 84873856660 scopus 로고
    • Navier-Stokes Computational Analysis of the B-1A Escape Capsule
    • January
    • Habchi, S.D., Hufford, G.S., and Marquette, T., "Navier-Stokes Computational Analysis of the B-1A Escape Capsule," AIAA-95-0187, January 1995.
    • (1995) AIAA-95-0187
    • Habchi, S.D.1    Hufford, G.S.2    Marquette, T.3
  • 5
    • 84873853404 scopus 로고
    • Validation of CFD Methodology for Ejection Seat Applications
    • January
    • Hufford, G.S. and Habchi, S.D., "Validation of CFD Methodology for Ejection Seat Applications," AIAA-94-0751, January 1994.
    • (1994) AIAA-94-0751
    • Hufford, G.S.1    Habchi, S.D.2
  • 6
    • 84873837388 scopus 로고    scopus 로고
    • A Computational Methodology for the Rapid Simulation of Jettisoned Aircraft Canopy Trajectories
    • January
    • Rock, S.G., Habchi, S.D., and Marquette, T.J., "A Computational Methodology for the Rapid Simulation of Jettisoned Aircraft Canopy Trajectories," AIAA-97-0169, January 1997.
    • (1997) AIAA-97-0169
    • Rock, S.G.1    Habchi, S.D.2    Marquette, T.J.3
  • 7
    • 84983119844 scopus 로고    scopus 로고
    • A Fully Automated Chimera Methodology for Multiple Moving Body Problems
    • January
    • Wang, ZJ. Parthasarathy, V., and Hariharan, N., "A Fully Automated Chimera Methodology for Multiple Moving Body Problems," AIAA-98-0217, January 1998.
    • (1998) AIAA-98-0217
    • Wang, Z.J.1    Parthasarathy, V.2    Hariharan, N.3
  • 8
    • 84983198411 scopus 로고    scopus 로고
    • CFD Research Corporation, CFD-FASTRAN User's Manual; Theory Manual, 1998
    • CFD Research Corporation, CFD-FASTRAN User's Manual; Theory Manual, 1998.
  • 12
    • 24944475831 scopus 로고
    • A Fully Conservative Structured/ Unstructured Chimera Grid Scheme
    • January
    • Wang, Z.J., "A Fully Conservative Structured/ Unstructured Chimera Grid Scheme," AIAA Paper 95-0671, January, 1995.
    • (1995) AIAA Paper 95-0671
    • Wang, Z.J.1
  • 13
  • 14
    • 84983107133 scopus 로고
    • Aerodynamic Characteristics of a 0.5-Scale Crewman/Ejection Seat model During a Simulated ejection from an F-16 Fighter at Free-Stream Mach Numbers from 0.4 to 1.2
    • October
    • Reichenau, D.E.A., "Aerodynamic Characteristics of a 0.5-Scale Crewman/Ejection Seat model During a Simulated ejection from an F-16 Fighter at Free-Stream Mach Numbers from 0.4 to 1.2," AEDC-TSR 78-P42, October 1978.
    • (1978) AEDC-TSR 78-P42
    • Reichenau, D.E.A.1
  • 15
    • 84983138652 scopus 로고
    • F-18 Automated Aircrew Escape System Sled Test
    • March
    • Murphy, J. V., and Jones, R.A., "F-18 Automated Aircrew Escape System Sled Test," MDC Report A5688, March 1979.
    • (1979) MDC Report A5688
    • Murphy, J.V.1    Jones, R.A.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.