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Abstract
Using an In-House Developed Computational Fluid Dynamics (Cfd) Software, Paras-3D,
Full Engine Simulation of a Scramjet Engine (Along With Cone Cylinder Fore-Body) Is Carried Out,
Burning Hydrogen as Fuel. This Paper Describes the Results of Cfd Simulations at Two Different
Mach Numbers and Equivalence Ratios and Comparison With the Flight Measured Engine
Pressure. Pressure Rise Due to Supersonic Combustion Captured by Computational Method Has
Very Good Agreement With Flight Measured Pressure Data. This Brings Good Confidence in The
Usage of Cfd Tools for Scramjet Engine Performance Prediction.
Keywords
Article Details
References
- Charles, E., Cockrell, Jr. and Walter C. Engelund., "Integrated Aero-propulsive Computational Fluid Dynamics Methodology for the Hyper-X Flight Experiment", Journal of Spacecraft and Rockets, Vol.38, No.6, November-December, 2001.
- Gnanasekar, S., Ashok,V., Dipankar Das and Lazar T. Chitilappilly., "Effect of Connected Pipe Test Conditions on Scramjet Combustor Performance", International Journal of Aerospace Innovations, Vol.1, No.4, December, 2009.
- Liu, J. and Gruber, M., "Preliminary Preflight CFD study on the HIFiRE Flight 2 Experiment", AIAA Paper, 2011-2204.
- Amit Kumar Singh., Gnanaseka,r S., Dipankar Das., Ashok, V. and Lazar T. Chitilappilly., "Full Engine Flow Simulation of Scramjet Engine and Effect of Fuel Equivalence Ratio", Space Transportation Systems (STS) Conference, 16-18, Decembe, 2011, Thiruvananthapuram.
- Lazar T. Chitilappilly., Sivarama Panicker, V. K., Jacob, P.C., Panicker, C. and Sivan, K., "Successful Flight Testing of Scramjet Engine Over Wide Range of Test Conditions", 68th International Astronautical Congress (IAC), 25-29, September 2017, Adelaide, Australia.
- Dmitry Davidenko., Iskender Gokalp., Emmanuel Dufour and Philippe Magre., "Numerical Simulation
- of Hydrogen Supersonic Combustion and Validation of Computational Approach", 12th AIAA International Space Planes and Hypersonic Systems and Technologies, December 2003, AIAA Paper 2003- 7033.
References
Charles, E., Cockrell, Jr. and Walter C. Engelund., "Integrated Aero-propulsive Computational Fluid Dynamics Methodology for the Hyper-X Flight Experiment", Journal of Spacecraft and Rockets, Vol.38, No.6, November-December, 2001.
Gnanasekar, S., Ashok,V., Dipankar Das and Lazar T. Chitilappilly., "Effect of Connected Pipe Test Conditions on Scramjet Combustor Performance", International Journal of Aerospace Innovations, Vol.1, No.4, December, 2009.
Liu, J. and Gruber, M., "Preliminary Preflight CFD study on the HIFiRE Flight 2 Experiment", AIAA Paper, 2011-2204.
Amit Kumar Singh., Gnanaseka,r S., Dipankar Das., Ashok, V. and Lazar T. Chitilappilly., "Full Engine Flow Simulation of Scramjet Engine and Effect of Fuel Equivalence Ratio", Space Transportation Systems (STS) Conference, 16-18, Decembe, 2011, Thiruvananthapuram.
Lazar T. Chitilappilly., Sivarama Panicker, V. K., Jacob, P.C., Panicker, C. and Sivan, K., "Successful Flight Testing of Scramjet Engine Over Wide Range of Test Conditions", 68th International Astronautical Congress (IAC), 25-29, September 2017, Adelaide, Australia.
Dmitry Davidenko., Iskender Gokalp., Emmanuel Dufour and Philippe Magre., "Numerical Simulation
of Hydrogen Supersonic Combustion and Validation of Computational Approach", 12th AIAA International Space Planes and Hypersonic Systems and Technologies, December 2003, AIAA Paper 2003- 7033.