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Volumn 43, Issue 1, 2006, Pages 125-131

Constant altitude-constant Mach number cruise range of transport aircraft with compressibility effects

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; APPROXIMATION THEORY; AVIATION; FLIGHT DYNAMICS; FUEL CONSUMPTION;

EID: 33644635797     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.14252     Document Type: Article
Times cited : (8)

References (20)
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  • 2
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    • Comparison of generalized approximate cruise range solutions for turbojet/fan aircraft
    • Cavcar, M., and Cavcar, A., "Comparison of Generalized Approximate Cruise Range Solutions for Turbojet/Fan Aircraft," Journal of Aircraft, Vol. 40, No. 5, 2003, pp. 891-895.
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    • Cavcar, M.1    Cavcar, A.2
  • 3
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    • Approximate solutions of range for constant altitude-constant high subsonic speed flight of transport aircraft
    • Cavcar, A., and Cavcar, M., "Approximate Solutions of Range for Constant Altitude-Constant High Subsonic Speed Flight of Transport Aircraft," Aerospace Science and Technology, Vol. 8, No. 6, 2004, pp. 557-567.
    • (2004) Aerospace Science and Technology , vol.8 , Issue.6 , pp. 557-567
    • Cavcar, A.1    Cavcar, M.2
  • 4
    • 0031131484 scopus 로고    scopus 로고
    • Cruise performance and range prediction reconsidered
    • Torenbeek, E., "Cruise Performance and Range Prediction Reconsidered," Progress in Aerospace Sciences, Vol. 33, No. 5-6, 1997, pp. 285-321.
    • (1997) Progress in Aerospace Sciences , vol.33 , Issue.5-6 , pp. 285-321
    • Torenbeek, E.1
  • 5
    • 0242373653 scopus 로고    scopus 로고
    • Airplane performance: Range and endurance
    • Dept. of Aerospace Engineering, Indian Inst. of Science, Bangalore, India, Dec.
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    • (2000) Fluid Mechanics Rept. 200 FM , vol.16
    • Ananthasayanam, M.R.1
  • 6
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    • Shevell, R.S.1
  • 9
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    • Pratt and Whitney Canada, Inc., Longueuil, QC, Canada
    • "JT15D-5 Fact Sheet," Pratt and Whitney Canada, Inc., Longueuil, QC, Canada, 1988.
    • (1988) JT15D-5 Fact Sheet
  • 11
    • 0003670229 scopus 로고
    • Longmans, Green and Co., London
    • Hilton, W. F., High Speed Aerodynamics, Longmans, Green and Co., London, 1952, pp. 47-49.
    • (1952) High Speed Aerodynamics , pp. 47-49
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  • 12
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  • 15
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    • Optimization of constant altitude-constant airspeed flight for piston-prop aircraft
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  • 17
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.