References
- An, C.H., Kang, D.W., Baek, S.T., Myong, R.S., Kim, W.C., and Choi, S.M., “Analysis of Plume Infrared Signatures of S-Shaped Nozzle Configurations of Aerial Vehicle,” Journal of Aircraft, Vol. 53, No. 6, pp. 1768-1778, 2016. https://doi.org/10.2514/1.C033685
- Rao, G.A. and Mahulikar, S.P., “New Criterion for Aircraft Susceptibility to Infrared Guided Missiles,” Aerospace Science and Technology, Vol. 9, No. 8, pp. 701-712, 2005. https://doi.org/10.1016/j.ast.2005.07.005
- Miller, E.H., Protopapas, J., Obye, R., and Wooten, W., "Nozzle Design and Integration in an Advanced Supersonic Fighter," Aircraft Systems and Technology Meeting, New York, U.S.A., p. 1813, Aug. 1979.
- Mahulikar, S.P., Sonawane, H.R., and Rao, G.A., “Infrared Signature Studies of Aerospace Vehicles,” Progress in Aerospace Science, Vol. 43, No. 7, pp. 218-245, 2007. https://doi.org/10.1016/j.paerosci.2007.06.002
- Spang III, H.A. and Brown, H., "Control of jet engines," Control Engineering Practice, Vol. 79, Issue. 9, pp. 1043-1059, 1999. https://doi.org/10.1016/S0967-0661(99)00078-7
- Sun, X.L., Wang, Z.X., Zhou, L., Liu, Z.W., and Shi, J.W., “Influences of Design Parameters on a Double Serpentine Convergent Nozzle,” Journal of Engineering for Gas Turbines and Power, Vol. 138, No. 7, pp. 072301, 2016. https://doi.org/10.1115/1.4032338
- Jaiswal, G. K., Rao, N., Kushari, A., "IR Signature Studies of Serpentine Nozzle," 7th International conference on theoretical, Applied, Computational and Experimental Mechanics, IIT Kharagpur, India, p. 158, Dec. 2017.
- "nEUROn," retrieved 15 Dec. 2018 from http://dassault-aviation.com.
- Cheng, W., Wang, Z., Zhou, L., Sun, X., and Shi, J., "Influences of Serpentine Ratio on the Infrared Signature of Serpentine Nozzle," Aerospace Science and Technology, Vol. 71, pp. 299-311, 2017. https://doi.org/10.1016/j.ast.2017.09.001
- Kim, T., Lee, H., Bae, J.Y., Kim, T., Cha, J., Jung, D., and Cho, H.H., "Susceptibility of Combat Aircraft Modeled as an Anisotropic Source of Infrared Radiation," IEEE Transactions on Aerospace and Electronic Systems, Vol. 52, No. 5, pp. 2467-2476, 2010. https://doi.org/10.1109/TAES.2016.150513
- Sun, X.L., Wang, Z.X., Zhou, L., Shi, J.W., and Liu, Z.W., "Experimental and Computational Investigation of Double Serpentine Nozzle," Journal of Aerospace Engineering, Vol. 229, Issue 11, pp. 2035-2050, 2014.
- Daniel E.E. and Erik, A.L., "Exhaust Nozzle Cooling Scheme for Gas Turbine Engine," U.S. Patent No. 5,577,381. 26, Nov. 1996.
- GasTurb 12, "GasTurb 12: Design and Off-Design Performance of Gas Turbines," GasTurb GmbH, Aachen, Germany, 2015.
- ANSYS Fluent V17.2, "ANSYS Fluent Theory Guide 17.2," ANSYS, Inc., Canonsburg, P.A., U.S.A., 2015.
- RadthermIR 10.4, "RadthermIR User Manual Version: 10.4.0," ThermoAnalyics, Inc., Calumet City, U.S.A., 2012.