Investigation of Aircraft Plume IR Signature for Various Nozzle Configurations and Atmospheric Conditions
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[1] Frederick S. Simmons,et al. Rocket Exhaust Plume Phenomenology , 2000 .
[2] Craig A. Hunter,et al. Experimental Investigation of Separated Nozzle Flows , 2004 .
[3] Rho-Shin Myong,et al. Computational Investigation of the Effect of Various Flight Conditions on Plume Infrared Signature , 2013 .
[4] R. Decher,et al. Infrared emissions from turbofans with high aspect ratio nozzles , 1981 .
[5] F. X. Kneizys,et al. Users Guide to LOWTRAN 7 , 1988 .
[6] Dong-Woo Kang,et al. Computational Investigation of the Effect of UAV Engine Nozzle Configuration on Infrared Signature , 2013 .
[7] Won-Cheol Kim,et al. A Study on the Effect of Engine Nozzle Configuration on the Plume IR Signature , 2012 .
[8] David Lynch,et al. Introduction to RF stealth , 2004 .
[9] W. Grosshandler. Radcal: A Narrow-Band Model for Radiation Calculations in a Combustion Environment , 2018 .
[10] Shripad P. Mahulikar,et al. Effect of Atmospheric Transmission and Radiance on Aircraft Infrared Signatures , 2005 .
[11] Shripad P. Mahulikar,et al. Aircraft Plume Infrared Signature in Nonafterburning Mode , 2005 .
[12] Robert E. Ball,et al. The fundamentals of aircraft combat survivability analysis and design , 1985 .