| Prediction and validation of Mars Pathfinder hypersonic aerodynamic database PA Gnoffo, RD Braun, KJ Weilmuenster, RA Mitcheltree, WC Engelund, ... Journal of Spacecraft and Rockets 36 (3), 367-373, 1999 | 100 | 1999 |
| Aerodynamic database development for the hyper-X airframe-integrated scramjet propulsion experiments WC Engelund, SD Holland, CE Cockrell Jr, RD Bittner Journal of Spacecraft and Rockets 38 (6), 803-810, 2001 | 95 | 2001 |
| Aerodynamic configuration design using response surface methodology analysis WC Engelund, DO Stanley, RA Lepsch, MM McMillin, R Unal NASA STI/Recon Technical Report A 94, 10718, 1993 | 87 | 1993 |
| Hyper-X research vehicle experimental aerodynamics test program overview SD Holland, WC Woods, WC Engelund Journal of spacecraft and rockets 38 (6), 828-835, 2001 | 81 | 2001 |
| Mars Pathfinder six-degree-of-freedom entry analysis RD Braun, RW Powell, WC Engelund, PA Gnoffo, KJ Weilmuenster, ... Journal of Spacecraft and Rockets 32 (6), 993-1000, 1995 | 78 | 1995 |
| Aerothermoelastic analysis of a NASP demostrator model J Heeg, T ZEILER, A POTOTZKY, C SPAIN, W ENGELUND 34th Structures, Structural Dynamics and Materials Conference, 1366, 1993 | 70 | 1993 |
| Approximation model building and multidisciplinary design optimization using response surface methods R Unal, R Lepsch, W Engelund, D Stanley 6th Symposium on Multidisciplinary Analysis and Optimization, 4044, 1996 | 64 | 1996 |
| Rocket-powered single-stage vehicle configuration selection and design DO Stanley, WC Engelund, RA Lepsch, M McMillin, KE Wurster, ... Journal of spacecraft and rockets 31 (5), 792-798, 1994 | 62 | 1994 |
| Propulsion system airframe integration issues and aerodynamic database development for the Hyper-X flight research vehicle WC Engelund, SD Holland, CE Cockrell Jr, RD Bittner XIV ISOABE, 1999 | 58 | 1999 |
| Integrated aeropropulsive computational fluid dynamics methodology for the Hyper-X flight experiment CE Cockrell Jr, WC Engelund, RD Bittner, TN Jentink, AD Dilley, A Frendi Journal of spacecraft and rockets 38 (6), 836-843, 2001 | 56 | 2001 |
| Mars entry atmospheric data system modeling and algorithm development R Beck, C Karlgaard, S O'Keefe, P Siemers, B White, W Engelund, ... 41st AIAA Thermophysics Conference, 3916, 2009 | 43 | 2009 |
| Entry, Descent, and Landing Roadmap Technology Area 09 M Adler, M Wright, C Campbell, I Clark, W Engelund, T Rivellini URL http://www. nasa. gov/pdf/501326main TA09-ID rev5 NRC wTASR. pdf, 2012 | 38 | 2012 |
| Entry, descent and landing systems analysis study: phase 2 report on exploration feed-forward systems AM Dwyer Ciancolo, JL Davis, WC Engelund, DR Komar, EM Queen, ... | 37 | 2011 |
| Hyper-X aerodynamics: the X-43A airframe-integrated scramjet propulsion flight-test experiments WC Engelund Journal of Spacecraft and Rockets 38 (6), 801-802, 2001 | 32 | 2001 |
| Integrated aero-propulsive CFD methodology for the Hyper-X flight experiment C Cockrell, Jr, W Engelund, A Dilley, R Bittner, T Jentink, A Frendi 18th Applied Aerodynamics Conference, 4010, 2000 | 30 | 2000 |
| Six-degree-of-freedom entry dispersion analysis for the METEOR recovery module PN Desai, RD Braun, RW Powell, WC Engelund, PV Tartabini Journal of Spacecraft and Rockets 34 (3), 334-340, 1997 | 29 | 1997 |
| NASA's human lunar landing strategy G Chavers, N Suzuki, M Smith, L Watson-Morgan, SW Clarke, ... International Astronautical Congress, 2019 | 27 | 2019 |
| Wind tunnel testing, flight scaling and flight validation with Hyper-X C McClinton, R Voland, S Holland, W Engelund, J White, J Pahle 20th AIAA Advanced Measurement and Ground Testing Technology Conference, 2866, 1998 | 24 | 1998 |
| Hyper-X wind tunnel program C McClinton, S Holland, K Rock, W Engelund, R Voland, L Huebner, ... 36th AIAA Aerospace Sciences Meeting and Exhibit, 553, 1998 | 24 | 1998 |
| Rarefied aerothermodynamic predictions for Mars global surveyor RG Wilmoth, DF Rault, FM Cheatwood, WC Engelund, RW Shane Journal of Spacecraft and Rockets 36 (3), 314-322, 1999 | 21 | 1999 |
