| Review of Infrared signature suppression systems using optical blocking method N Baranwal, SP Mahulikar Defence Technology 15 (3), 432-439, 2019 | 60 | 2019 |
| Infrared signature of aircraft engine with choked converging nozzle N Baranwal, SP Mahulikar Journal of thermophysics and heat transfer 30 (4), 854-862, 2016 | 35 | 2016 |
| Aircraft engine's infrared lock-on range due to back pressure penalty from choked convergent nozzle N Baranwal, SP Mahulikar Aerospace Science and Technology 39, 377-383, 2014 | 29 | 2014 |
| IR signature study of aircraft engine for variation in nozzle exit area N Baranwal, SP Mahulikar Infrared Physics & Technology 74, 21-27, 2016 | 18 | 2016 |
| Infrared Signature of Combat Aircraft Incorporating Weight Penalty due to the Divergent Section of the Convergent-Divergent Nozzle N Baranwal, SP Mahulikar SAE Technical Paper, 2021 | 2 | 2021 |
| Analytical Estimation of Infrared Signature of Converging and Converging-Diverging Nozzles of Jet Engine N Baranwal, SP Mahulikar SAE International Journal of Aerospace 14 (2), 2021 | 1 | 2021 |
| Infrared Signature of Fixed and Variable Area CD Nozzle of Aircraft Engine N Baranwal, SP Mahulikar SAE International Journal of Aerospace 16 (01-16-02-0011), 165-176, 2023 | | 2023 |
| Performance Comparison of Rectangular Nozzle with Circular Nozzle of Military Aircraft Engine BN Menon D, Shivam VS, Veerendra TU, Raikar A Materials Today: Proceedings, 2022 | | 2022 |
| Infrared signature of jet nozzle in off-design operation of combat aircraft engine (PhD) N Baranwal IITMandi, 2018 | | 2018 |
