| Parametric cycle analysis of adaptive cycle engine HR Patel Masters Thesis, 16, 2016 | 15 | 2016 |
| Parametric cycle analysis of adaptive cycle engine HR Patel, D Wilson 2018 joint propulsion conference, 4521, 2018 | 9 | 2018 |
| Strategic Forecasting Toward Achieving Defensible Space Architecture by Year 2030 H Patel, IW Maynard, L Rana, B Chudoba Journal of spacecraft and rockets 59 (5), 1437-1454, 2022 | 4 | 2022 |
| 2D Mixed-Compression Inlet Sizing of Supersonic Vehicles JA Medina, H Patel, B Chudoba AIAA AVIATION 2021 FORUM, 2780, 2021 | 4 | 2021 |
| Inlet sizing of hypersonic vehicles for conceptual design JA Medina, H Patel, B Chudoba ASCEND 2021, 4096, 2021 | 3 | 2021 |
| Performance evaluation and flame stabilization of stagnation point reverse flow combustor R Manjunath, PH Rajendrabhai, MDZ Quadri, SS Srinivas International Journal of Research in Engineering and Technology 4, 2015 | 2 | 2015 |
| Conceptual Design Level Airframe/Propulsion Integration Using the Generic Synthesis Framework AVDS: Application to Supersonic and Hypersonic Aerospace Vehicles H Patel The University of Texas at Arlington, 2022 | 1 | 2022 |
| A Sizing Study Comparison of Hypersonic Demonstrator Vehicles with a Pre-Cooled Turbojet Cycle HR Patel, B Chudoba 23rd AIAA International Space Planes and Hypersonic Systems and Technologies …, 2020 | 1 | 2020 |
| Sizing of LEVCON surface for turn performance and controllability RG Pillai, HR Patel AIAA Aviation 2019 Forum, 2800, 2019 | 1 | 2019 |
| Conceptual Design level Airframe/Propulsion Integration Using the Generic Synthesis Framework AVDS. H Patel | | 2023 |
