Thermal state of the shell for supersonic part of the ramjet nozzle-Reference-Cited by-同舟云学术

Thermal state of the shell for supersonic part of the ramjet nozzle

Published:2017-04 Issue:2 Volume:60 Page:236-242
ISSN:1068-7998
Container-title:Russian Aeronautics
language:en
Short-container-title:Russ. Aeronaut.

Author:

Zarubin G. P.,Zimin V. N.,Kuvyrkin G. N.

Publisher

Allerton Press

Subject

Aerospace Engineering

Link

http://link.springer.com/content/pdf/10.3103/S106879981702012X.pdf

Reference16 articles.

1. Aleksandrov, V.Yu., Aref’ev, K.Yu., and Voronetskii, A.V., Efficiency Analysis of the Regenerative Cooling System for Supersonic Ramjet on Hydrocarbon Fuel, Teplovye Protsessy v Tekhnike, 2014, no. 11, pp. 489–495.

2. Kartovitskii, L.L., Levin, V.M., and Yakovlev, A.A., A Concept of Increasing Efficiency for Ramjet Operation, Izv.Vuz. Av. Tekhnika, 2015, vol. 58, no. 4, pp. 67–72 [Russian Aeronautics (Engl. Transl.), vol. 58, no. 4, pp. 431–437].

3. Gubertov, A.M., Koshlakov, V.V., Mironov, R.V., Rubinskii, V.V., et al., Long-Run Firing Tests of Rocket Engine Nozzles Based on Carbon Composites, Izv. RAN. Energetika, 2012, no. 5, pp. 124–130.

4. Zarubin, V.S., The Equilibrium Temperature of the Uncooled Muzzle Envelope for Liquid Rocket Engine Nozzle, Inzhenernyi Zhurnal: Nauka i Innovatsii, 2013, vol. 20, no. 8, pp. 11–20.

5. Baskakov, V.N., Volkov, L.I., Kalinin, S.V., and Tsatsuev, S.M., Modeling of Heat Erosion Resistance of Carbon-Carbon and Ceramic Matrix Composite Materials for High Energy Propulsion Applications, Izv.RAN. Energetika, 2015, no. 3, pp. 64–71.

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