Numerical simulation of throttling processes in the ramjet engine

Author:

Nechiporuk S.Yu.1,Zaripov D.Kh.1

Affiliation:

1. Bauman Moscow State Technical University

Abstract

Aimed at determining the maximum allowable pressure in the combustion chamber causing no flow separation in the air intake device, numerical simulation of the throttling process in a ramjet engine was carried out. Calculations were made in two formulations: with local and global time steps. When comparing results obtained using these approaches, the possibility was found to determine the air intake device throttling characteristics without losing the accuracy at the initial stages of designing the ramjet engines with introduction of the local time step. The non-stationary model created the basis for selecting the optimal integration step to minimize computational resources. The flow pulsations period was evaluated for the event of a surge. These pulsations frequencies were registered in the extremely low frequency range.

Publisher

Bauman Moscow State Technical University

Subject

General Medicine

Reference10 articles.

1. Gunko Yu.P., Mazhul I.I., Nurutdinov V.I. Chislennoye issledovanie razrusheniya sverkhzvukovogo potoka pri drosselirovanii kanala vozdukhozabornika [Numerical study of the supersonic flow breakup during the intake channel throttling]. Teplofizika i aeromekhanika — Thermal Physics and Aeromechanics, 2014, vol. 21, no. 2, pp. 163–178.

2. Lyubimov D.A., Chestnykh A.O. Analiz RANS/ILES metodom vliyaniya drosselirovaniya na techenie v vozdukhozabornike smeshannogo szhatiya pri bolshikh sverkhzvukovykh skorostyakh [RANS/ILES analysis by the throttling effect method on the flow in a mixed-compression air intake at the high supersonic speeds]. Sixth International school-seminar. Evpatoria, June 5–12, 2016, Russian Academy of Sciences, Zhukovsky Central Aerohydrodynamic Institute. Moscow, Zhukovsky Central Aerohydrodynamic Institute Publ., 2016, pp. 103–104.

3. Lyubimov D.A., Chestnykh A.O. Analiz RANS/ILES metodom vliyaniya ugla ataki i drosselirovaniya na uroven i spektralnye svoistva pulsatsiy davleniya v vysokoskorostnom vozdukhozabornike [RANS/ILES analysis by the method of the angle of attack and throttling effect on the pressure pulsations level and spectral properties in the high-speed air intake device]. Tezisy dokladov Shestoy Otkrytoy vserossiyskoy (vosemnadtzatoy nauchno-tekhniceskoy) konferentsii po aerodinamike [Abstracts, The Sixth All-Russian (The eighteenth scientific and technical) Conference on Aerodynamics]. Moscow, September 22–27, 2019, Zhukovsky Central Aerohydrodynamic Institute. Moscow, Zhukovsky Central Aerohydrodynamic Institute Publ., 2019, pp. 282–283.

4. Karasev V.N., Kartovitsky L.L., Levin V.M. Voprosy organizatsii rabochego protsessa v kamere sgoraniya PVRD [Issues of the operation process organization in the ramjet combustion chamber]. Vestnik Moskovskogo aviatsionnogo instituta — Aerospace MAI Journal, 2009, vol. 16, no. 5, 10 p.

5. Lyubimov D.A., Chestnykh A.O. Issledovanie RANS/ILES metodom techeniya v vysokoskorostnom vozdukhozabornike smeshannogo szhatiya na razlichnykh rezhimakh raboty [RANS/ILES study by the flow method in a high-velocity mixed-compression air intake device at various operating modes]. Teplofizika vysokikh temperatur — High Temperature, 2018, vol. 56, no. 5, pp. 764–776.

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3