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Performance of Two Types of High Speed, High Efficiency ‎Axisymmetric Intakes

Publish place: Journal of Applied and Computational Mechanics، Vol: 7، Issue: 1
Publish Year: 1400
نوع سند: مقاله ژورنالی
زبان: English
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https://civilica.com/doc/1222020

شناسه ملی سند علمی:

JR_JACM-7-1_010

تاریخ نمایه سازی: 9 خرداد 1400

Abstract:

Performance of two axisymmetric air intakes are compared at conditions suitable for Mach number range from ۲ to ۸. First is the Busemann intake and second is the reversed isentropic nozzle. The isentropic nozzle is built by the method of characteristics. The contour of this nozzle is taken as a compression surface for the incoming flow. Performances of these two intakes are compared by comparison of both viscous and inviscid CFD calculations at Mach ۶. Viscous flow calculations show that the total pressure recovery in compression section is ۰.۸۳۱۶ in the Busemann intake and ۰.۸۶۹ in the reversed isentropic nozzle intake.

Keywords:

supersonic , air intake , near-isentropic compression , Total pressure recovery‎

Authors

Vladislav Galkin

School of Earth Sciences & Engineering, Tomsk Polytechnic University, ۶۳۴۰۵۰, Tomsk, Russia

Vasily Fomin

Khristianovich Institute of Theoretical and Applied Mechanics of the Siberian Branch of the Russian Academy of Sciences,‎ ‎۶۳۰۰۹۰, Novosibirsk, Russia

Sannu Mölder

Ryerson University, ON M۵B ۲K۳, Toronto, Canada‎

Dmitry Vnuchkov

Khristianovich Institute of Theoretical and Applied Mechanics of the Siberian Branch of the Russian Academy of Sciences,‎ ‎۶۳۰۰۹۰, Novosibirsk, Russia

Valery Zvegintsev

Khristianovich Institute of Theoretical and Applied Mechanics of the Siberian Branch of the Russian Academy of Sciences,‎ ‎۶۳۰۰۹۰, Novosibirsk, Russia

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