EVALUATION OF FLIGHT PATH MAIN SECTIONS AND IMPOSED RESTRICTIONS ON THE COMPATIBILITY OF AIRCRAFT ENGINE AND FRAME

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ASADOLLAHI GHOHYEH A.; INANLOO M.A.

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Journal Paper

Paper Information

Journal: JOURNAL OF AEROSPACE SCIENCE AND RESEARCH Year:2009 | Volume:2 | Issue:2 Page(s): 49-58

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Information Journal Paper

Title

EVALUATION OF FLIGHT PATH MAIN SECTIONS AND IMPOSED RESTRICTIONS ON THE COMPATIBILITY OF AIRCRAFT ENGINE AND FRAME

Author(s)

ASADOLLAHI GHOHYEH A. | INANLOO M.A. | Issue Writer Certificate

Keywords

TAKE OFFQ3

LANDINGQ3

AIRCRAFT ENGINEQ2

WINGQ2

Abstract

It is of great significance to assure the compatibility between AIRCRAFT ENGINE and frame within the basic design and prior to model fabrication and costly experiments. The main purpose of this research was the evaluation of flight path main sections and imposed restrictions in the compatibility of engine and frame. Results show methods to decrease take- off run, noise level, etc., identified through an analytical approach.

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APA: Copy

ASADOLLAHI GHOHYEH, A., & INANLOO, M.A.. (2009). EVALUATION OF FLIGHT PATH MAIN SECTIONS AND IMPOSED RESTRICTIONS ON THE COMPATIBILITY OF AIRCRAFT ENGINE AND FRAME. JOURNAL OF AEROSPACE SCIENCE AND RESEARCH, 2(2), 49-58. SID. https://sid.ir/paper/199474/en

Vancouver: Copy

ASADOLLAHI GHOHYEH A., INANLOO M.A.. EVALUATION OF FLIGHT PATH MAIN SECTIONS AND IMPOSED RESTRICTIONS ON THE COMPATIBILITY OF AIRCRAFT ENGINE AND FRAME. JOURNAL OF AEROSPACE SCIENCE AND RESEARCH[Internet]. 2009;2(2):49-58. Available from: https://sid.ir/paper/199474/en

IEEE: Copy

A. ASADOLLAHI GHOHYEH, and M.A. INANLOO, “EVALUATION OF FLIGHT PATH MAIN SECTIONS AND IMPOSED RESTRICTIONS ON THE COMPATIBILITY OF AIRCRAFT ENGINE AND FRAME,” JOURNAL OF AEROSPACE SCIENCE AND RESEARCH, vol. 2, no. 2, pp. 49–58, 2009, [Online]. Available: https://sid.ir/paper/199474/en

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