STUDY OF IMPORTANT VARIABLES OF AERODYNAMICS FOR SUBSONIC AIRCRAFT USING ADVANCED AIRCRAFT ANALYSIS SOFTWARE

محتوى المقالة الرئيسي

Asaad T. Al-Omran
Sattar J. Habeeb
Israa Yheaa Daood

الملخص

This study presents the important variables of aerodynamics of subsonic aircraft using AAA software, moreover to comprehensive preview of some imperical and mathematical equations where needs in this analysis process. Cruise mission chose for this study comparing with another mission of flight such as Take-off, Climb, Dive & Descent, and Landing according to important of the mission and cruise mission has large rung during the flight mission. These analyses of process submit to more and complex iteration process until we access to correct solution. Lift, drag, and moment coefficients along the lift surfaces such as wing, and horizontal tail were showed. Also this paper explain the effect of flight level, aircraft speed, aspect ratio of lift surfaces on lift curve. Results show that, increase the value of altitude, load factor,aspect ratio leads to increase the value of lift coofficent and decrease the airplane velocity.

تفاصيل المقالة

كيفية الاقتباس
"STUDY OF IMPORTANT VARIABLES OF AERODYNAMICS FOR SUBSONIC AIRCRAFT USING ADVANCED AIRCRAFT ANALYSIS SOFTWARE" (2010) مجلة الهندسة, 16(01), ص 877–893. doi:10.31026/j.eng.2010.01.05.
القسم
Articles

كيفية الاقتباس

"STUDY OF IMPORTANT VARIABLES OF AERODYNAMICS FOR SUBSONIC AIRCRAFT USING ADVANCED AIRCRAFT ANALYSIS SOFTWARE" (2010) مجلة الهندسة, 16(01), ص 877–893. doi:10.31026/j.eng.2010.01.05.

تواريخ المنشور

المراجع

 Clancy, L.J., “ Aerodynamics “, A pitman International Text, 1975.

 Perkins, C.D., “ Airplane Performance Stability and Control “, John Wily and sans, Inc., 1976.

 Ramyer, D.P., “ Aircraft Design: A Conceptual Approach “, Second Edition, AIAA, Washington, 1992.

 Roskam, J., “ Airplane Design Part II “ , McGraw-Hill Book Company, ISBN 884885-43-8, 2003.

 Roskam, J., “ Airplane Design Part I “ , McGraw-Hill Book Company, ISBN 884885-42x, 2003.

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