[1] B. H. Park, J. H. Lee, W. Yoon, “Studies on the starting transient of a straight cylindrical supersonic diffuser: Effects of diffuser length and pre-evacuation state”, International Journal of Heat and Fluid Flow, Vol. 29, No. 5, pp. 1369–1379, 2008.#
H.W. Yeom, S. Yoon, Sung HG. “Flow dynamics at the minimum starting condition of a supersonic diffuser to simulate a rocket’s high altitude performance on the ground”. Journal of Mechanical Science and Technology. 2009 Jan 1;23(1):254-61.#
D.R. Jones, “Passive Rocket Diffuser Theory: A Re-Examination of Minimum Second Throat Size”, NASA Technical Memorandum, 2016-219219,2016.# [4] N. Fouladi, A. Mohamadi, H. Rezaei., “Numerical design and analysis of supersonic exhaust diffuser in altitude test simulator”. Modares Mechanical Engineering. 2016 Oct 15;16(8):159-68.(In Persian)# [5] N. Fouladi, M. Farahani,. “Numerical investigation of second throat exhaust diffuser performance with thrust optimized parabolic nozzles”, Aerospace Science and Technology, Volume 94, October 2020,
https://doi.org/10.1016/j.ast.2020.106020# [6] N. Fouladi, M. Farahani, A.R. Mirbabaei,. “Performance evaluation of a second throat exhaust diffuser withathrust optimized parabolic nozzle”, Aerospace Science and Technology, Volume 94, November2019.# [7] N. Fouladi, A, Mohamadi, H, Rezaei. “Numerical investigation of pre-evacuation influences of second throat exhaust diffuser”., Journal of fluid mechanics and aerodynamics, In press, 2017. (In Persian)# [8] E. Mohammadi, N. Fouladi, A. Madadi, “
Design and analysis of gas ejector in high altitude test facility”, Amirkabir Journal of Mechanical Engineering 52 (11), 3015-3032, 2019.# [9] R. Ashokkumar, S. Sankaran, K. Srinivasan, T. Sundararajan, “Effects of Vacuum Chamber andReverse Flow on SupersonicExhaust Diffuser Starting”, Journal of Propulsion and Power, Vol. 31, No. 2, pp. 750-754, 2015.# [10] N. Fouladi, Numerical investigation of backflow arrester influences on altitude test simulator starting performance”, Modares Mechanical Engineering,Vol. 17, No. 7, pp. 185-196, 2017. (in Persian)# [11] S. Sankaran, T.N.V. Satyanarayana, K. Annamalai, K. Visvanathan, V. Babu, T. Sundararajan, “CFD Analysis for Simulated Altitude Testing of Rocket Motors”, Canadian Aeronautics and Space Journal, Vol. 48, No. 2, pp.153-162, 2002.# [12] K. Annamalai, K. Visvanathan, V. Sriramulu, K.A. Bhaskaran, “Evaluation of the Performance of Supersonic Exhaust Diffuser Using Scaled Down Models”, Experimental Thermal and Fluid Science, Vol. 17, No. 3, pp. 217-229, 1998.# [13] B.H. Park, J.H. Lee, W. Yoon, “Studies on the Starting Transient of a Straight Cylindrical Supersonic Exhaust Diffuser: Effects of Diffuser Length and Pre-evacuation State”, International Journal of Heat and Fluid Flow, Vol. 29, No. 5, pp. 1369–1379, 2008.# [14] P. Wegener, and R. Lobb, “NOL Hypersonic Tunnel No. 4 Results II: Diffuser Investigation,” NAVORD Report 2376, May 1952.# [15] W. Jones, Price, H., and Lorenzo, C., “Experimental Study of Zero-Flow Ejectors Using Gaseous Nitrogen,” NASA TN D-203, March 1960.# [16] P. F. Massier, and E. J. Roschke, “Experimental Investigation of Exhaust Diffusers for Rocket Engines,” Jet Propulsion Lab., California Inst. of Technology, TR-32-210, Pasadena, CA, 1962.# [17] R. Bauer, and R. German, “The Effect of Second Throat Geometry on the Performance of Ejectors Without Induced Flow,” AEDC-TDR-61-133, November 1961. # [18] G.V.R. Rao, “Approximation of optimum thrust nozzle contour, ” ARS J. 30(6) 561, 1960.# [19] j. Ostlund, “supersonic flow separation with application to rocket engine nozzles, ” Technical report, 2004 # [20] M. Farajijalal, “Design and Fabrication of an Experimental Model of Higjh Altitude Simulation Thrust Stand”, MSc Thesis, Sharif Univ., Tehran, Iran, 2018.
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