Author:
Sankaran S.,Venkatesh G.,Ramakrishna V. V.,Anandaraj J.,Aditya B. N. V. S.,Deepthi M.
Publisher
Springer Nature Singapore
Reference8 articles.
1. Passive Rocket Diffuser Theory: A Re-Examination of Minimum Second Throat Size, Daniel R. Jones Stennis Space Center, Mississippi, NASA TM 2016-219219
2. Massier, P.F., Roschke, E.J., 1960. Experimental investigation of exhaust diffusers for rocket engines. NASA CR 51076.
3. Gothert, B.H. (1962). “High altitude and space simulation testing”. ARS J., pp. 872–882.
4. Annamalai, K., Visvanathan, K., Sriramulu, V., Bhaskaran, K.A., 1998. Evaluation of the performance of supersonic exhaust diffuser using scaled down models. Experimental Thermal and Fluid Science 17, 217–229.
5. Sankaran, S., Satyanarayana, T.V.V., Annamalai, K., Visvanathan, K., Babu, V., Sundararajan, T., 2002. CFD analysis for simulated altitude testing of rocket motors. Canadian Aeronautics and Space J 48 (2), 153–162.