| Forced motions design for aerodynamic identification and modeling of a generic missile configuration J Allen, M Ghoreyshi Aerospace Science and Technology 77, 742-754, 2018 | 29 | 2018 |
| Control device effectiveness studies of a 53∘ swept flying wing configuration. Experimental, computational, and modeling considerations P Löchert, KC Huber, M Ghoreyshi, J Allen Aerospace Science and Technology 93, 105319, 2019 | 12 | 2019 |
| Aerodynamic loads identification and modeling of UCAV configurations with control surfaces using prescribed CFD maneuvers JD Allen, M Ghoreyshi, A Jirasek, M Satchell 2018 Applied Aerodynamics Conference, 2999, 2018 | 10 | 2018 |
| Preliminary computational aerodynamic investigation of the NATO AVT-251 multi-disciplinary configuration P Aref, ST McGlone, J Allen, M Ghoreyshi, A Jirasek, AJ Lofthouse 35th AIAA Applied Aerodynamics Conference, 3412, 2017 | 5 | 2017 |
| Study of Exhaust Gas Reingestion BY Min, PO Bowles, AF Dunn, D Lamb, C Lian, J Frydman, BE Wake, ... AIAA Scitech 2021 Forum, 0030, 2021 | 3 | 2021 |
| Aerodynamic Identification and Modeling of Generic UCAV Configurations with Control Surface Integration JD Allen University of Colorado Colorado Springs, 2017 | 2 | 2017 |
| The CH-53K Exhaust Gas Reingestion Trade Study: Using a Tiered CFD Modeling Approach to Solving the EGR Challenges on the CH-53K King Stallion PO Bowles, JR Forsythe, BY Min, D Lamb, AF Dunn, E Siegel, J Frydman, ... AIAA Scitech 2021 Forum, 0031, 2021 | 1 | 2021 |
| Model Based Engine Exhaust Redesign and Evaluation on the CH-53K King Stallion D Lamb, PO Bowles, BY Min, C Lian, X Xie, J Frydman, G Harrington, ... AIAA Scitech 2021 Forum, 0139, 2021 | 1 | 2021 |
