DESIGN AND ANALYSIS OF A TURBOJET ANTI-ICE SYSTEM

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KARIMI ALI AKBAR; JAMSHIDI NAEINI M.J.; HAMIDI H.A.D.E.D.

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Journal: Journal of Aerospace Mechanics Year:2007 | Volume:3 | Issue:3 Page(s): 9-19

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Information Journal Paper

Title

DESIGN AND ANALYSIS OF A TURBOJET ANTI-ICE SYSTEM

Author(s)

KARIMI ALI AKBAR | JAMSHIDI NAEINI M.J. | HAMIDI H.A.D.E.D. | Issue Writer Certificate

Keywords

ANTI-ICINGQ3

CAPTURE AREAQ3

TURBOJETQ2

CONTROL SYSTEMQ3

Abstract

In this paper, an anti-ice system for a TURBOJET is designed. Speed, altitude, ambient temperature and moisture content of the air are considered in the design. Critical conditions, in which icing is expected, are determined. Capture region, where ice formation is most probable, is investigated and protected by hot air from compressor exit. A CONTROL SYSTEM based on PID controller is designed to control the flow rate of the hot air. In this design, surfaces like lip, bullet nose, and struts are protected against ice formation.

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APA: Copy

KARIMI, ALI AKBAR, JAMSHIDI NAEINI, M.J., & HAMIDI, H.A.D.E.D.. (2007). DESIGN AND ANALYSIS OF A TURBOJET ANTI-ICE SYSTEM. AEROSPACE MECHANICS JOURNAL, 3(3), 9-19. SID. https://sid.ir/paper/101741/en

Vancouver: Copy

KARIMI ALI AKBAR, JAMSHIDI NAEINI M.J., HAMIDI H.A.D.E.D.. DESIGN AND ANALYSIS OF A TURBOJET ANTI-ICE SYSTEM. AEROSPACE MECHANICS JOURNAL[Internet]. 2007;3(3):9-19. Available from: https://sid.ir/paper/101741/en

IEEE: Copy

ALI AKBAR KARIMI, M.J. JAMSHIDI NAEINI, and H.A.D.E.D. HAMIDI, “DESIGN AND ANALYSIS OF A TURBOJET ANTI-ICE SYSTEM,” AEROSPACE MECHANICS JOURNAL, vol. 3, no. 3, pp. 9–19, 2007, [Online]. Available: https://sid.ir/paper/101741/en

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