[1] J. Hall, “Optimized Dual Expander Aerospike Rocket”, Department of the Airforce Air University Airforce Instituite of Technology, US, Ohio, (2011).
[2] T. A. Ladeinde, Performance Comparison Between a Full-Length and a Truncated Aerospike Nozzle, Msc thesis Department of Mechanical and Aerospace Engineering, California State University, Long Beach, (2009).
[3] M. Nazarinia, A. Naghib-Lahouti, E. Tolouei, “Design and Numerical Analysis of Aerospike Nozzles with Different Plug Shapes to Compare their Performance with a Conventional Nozzle”, AIAC-11 Eleventh Australian International Aerospace Congress, Melbourne, Australia,13-17 March, (2005).
[4] E. Besnard, H. Chen, T. Mueller, and J. Garvey, “Design, Manufacturing and Test of aPlug Nozzle Rocket Engine”, Proceedings of the 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, (2002).
[5] E. S. Mcvay, “Design of a Dual-Expander Aerospike Nozzle Rocket Engine”, MSC Thesis,Department of Aerospace Engineering and Mechanics in the Graduate School of the University of Alabama, (2016).
[6] P. Lemieux, “Development of a Reusable Aerospike Nozzle for Hybrid Rocket Motors”, 39th AIAA Fluid Dynamics Conference, San Antonio, Texas, (2009).
[7] T. Karthikeyan, S. K. Aravindhkumar, J. Arun Kumar, “Design and Analysis of Aerospike Nozzle toImprove Thrust in Hybrid Rocket Engine”, International Journal of Engineering Trends and Techno logy, Vol. 36, No. 7, (2016).
[8] T. Niimi, H. Mori, K. Okabe, Y. M. Taniguchi, “Analyses of Flow Field Structures Around Linear-Type Aerospike Nozzles Using LIF and PSP”, 20th International Congress on Instrumentation in Aerospace Simulation Facilities, pp. 15-20, ( 2003).
[9] T. Wang, “Effect of Fence on Linear Aerospike Plume-Induced Base-Heating Physics”, Journal of Thermo physics and Heat Transfer, Vol. 14, No. 4, (2000).
[10] T. Zebbiche, Z. Youbi, “Supersonic Two-Dimensional Plug Nozzle Conception at High Temperature” , Emirates Journal for Engineering Research, Vol. 11, (2006).
[11] S. B. Verma, “Performance Characteristics of Annular Conical Aerospike Nozzle with Free stream Effect”, Journal of Propulsion and Power, Vol. 26, No. 3, (2009).
[12] A. Naghib-Lahouti, E. Tolouei, “Investigation of the Effect of Base Bleed on Thrust Performance of a Truncated Aaerospike Nozzle in Off-Design Conditions”, European Conference on Computational Fluid Dynamics, ECCOMAS CFD, Delft, Netherlands, (2006).
[13] A. Zilic, D. L. Hitt, and A. A. Alexeenko, “Numerical Simulations of Supersonic Flow in a Liear Aerospike Micronozzle”, 37th AIAA Fluid Dynamics Conference and Exhibit, 25-28 Jun, Miami, FL, (2007).
[14] T. W. Simpson, F. Mistree, “Multidisciplinary Approach to Linear Aerospike Nozzle Optimization”, AIAA journal, Vol. 39, No. 12, (2001).
[15] A. N. Kraiko, N. I. Tillyayeva, “Contouring Spike Nozzles and Determining the Optimal Direction of Their Primary Flows”, Journal of Fluid Dynamics,Vol. 42, No. 2, (2007).
[16] O. Bozic, D. Porrmann, “Estimation of Flow Field Properties and Thrust Performances of Axisymmetric Plug-Nozzles using CFD Simulations”, Turbulence, Heat and Mass Transfer 6, 14-18 September, Rome, Italy, (2009).
[17] M. Imran, “Introduction to Aerospike and its Aerodynamic Features”, International Journal of Scientific and Research Publications, Vol. 6, No. 5, (2016).
Send comment about this article