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Volumn , Issue , 1996, Pages 88-96

A numerical simulation study to develop an acceptable wake encounter boundary for A B737-100 airplane

Author keywords

[No Author keywords available]

Indexed keywords

AIR TRANSPORTATION; AIRCRAFT; DEGREES OF FREEDOM (MECHANICS); NASA; VORTEX FLOW; WAKES;

EID: 84982319093     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-3372     Document Type: Conference Paper
Times cited : (4)

References (12)
  • 3
    • 3342936245 scopus 로고
    • Wake Vortices-A Primer
    • Machol, R. E.: Wake Vortices-A Primer. FAA Aviation Safety Journal, Pages 16-19, Vol. 3, No. 1, 1993.
    • (1993) FAA Aviation Safety Journal , vol.3 , Issue.1 , pp. 16-19
    • Machol, R.E.1
  • 7
    • 0016036926 scopus 로고
    • Study of Control System Effectiveness in Alleviating Vortex Wake Upsets
    • March
    • Johnson, W. A., Teper, G. L., and Rediess, H. A., "Study of Control System Effectiveness in Alleviating Vortex Wake Upsets," Journal of Aircraft, Vol. 11, No. 3, March 1974, pp. 148-154.
    • (1974) Journal of Aircraft , vol.11 , Issue.3 , pp. 148-154
    • Johnson, W.A.1    Teper, G.L.2    Rediess, H.A.3
  • 10
    • 0028383696 scopus 로고
    • Required Navigation Performance (RNP) for Precision Approach and Landing with GNSS Application
    • Navigation:, No. 1, Spring
    • Kelly, R. J.; and Davis, J. M.: "Required Navigation Performance (RNP) for Precision Approach and Landing with GNSS Application," Navigation: Journal of The Institute of Navigation, Vol. 41, No. 1, Spring 1994.
    • (1994) Journal of The Institute of Navigation , vol.41
    • Kelly, R.J.1    Davis, J.M.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.