| On wings of the minimum induced drag: Spanload implications for aircraft and birds AH Bowers, OJ Murillo, RR Jensen, B Eslinger, C Gelzer | 101 | 2016 |
| An overview of the NASA F-18 high alpha research vehicle AH Bowers, JW Pahle, RJ Wilson, BC Flick, RL Rood High-Angle-of-Attack Technology, 1996 | 42 | 1996 |
| Multiaxis Thrust Vectoring Using Axisymmetric Nozzles and Postexit Vanes on an F/A-18 Configuration Vehicle AH Bowers, GK Noffz, SB Grafton, ML Mason, LR Peron High-Angle-of Attack Technology Conference, 1991 | 33 | 1991 |
| Thrust vectoring on the NASA F-18 high alpha research vehicle AH Bowers, JW Pahle High-Angle-of-Attack Technology Conference, 1996 | 25 | 1996 |
| Study of near-optimal endurance-maximizing periodic cruise trajectories PK Menon, GD Sweriduk, AH Bowers Journal of aircraft 44 (2), 393-398, 2007 | 24 | 2007 |
| Estimation of the longitudinal aerodynamic parameters from flight data for the NASA F/A-18 HARV M Napolitano, A Paris, B Seanor, A Bowers 21st Atmospheric Flight Mechanics Conference, 3419, 1996 | 23 | 1996 |
| Estimation of the lateral-directional aerodynamic parameters from flight data for the NASA F/A-18 HARV M Napolitano, A Paris, B Seanor, A Bowers 21st Atmospheric Flight Mechanics Conference, 3420, 1996 | 22 | 1996 |
| Flight, propulsion, and thermal control of advanced aircraft and hypersonic vehicles D White, A Bowers, K Iliff, G Noffz, M Gonda, J Menousek Handbook of Intelligent Control: Neural, Fuzzy, and Adaptive Approaches …, 1992 | 20 | 1992 |
| Generic hypersonic aerodynamic model example (GHAME) for computer simulation AH Bowers, KW Iliff NASA TM, NASA Ames-Dryden, Edwards, CA, 1987 | 13 | 1987 |
| A Generic Hypersonic Aerodynamic Model Example (GHAME) A Bowers, G Noffz, M Gonda, K Iliff NASA Dryden Flight Research Facility, 1989 | 11 | 1989 |
| Visualization and image processing of aircraft shock wave structures LM Weinstein, K Stacy, GJ Vieira, EA Haering Jr, AH Bowers 1st Pacific Symposium on Flow Visualization and Image Processing, Feb. 23-26 …, 1997 | 9 | 1997 |
| Parameter estimation for a cessna u-206 aircraft using the maximum likelihood method M Napolitano, A Paris, B Seanor, A Bowers 19th Atmospheric Flight Mechanics Conference, 3481, 1994 | 9 | 1994 |
| A comparison of Wortmann airfoil computer-generated lift and drag polars with flight and wind tunnel results AH Bowers, AG Sim | 9 | 1984 |
| On the Minimum Induced Drag of Wings AH Bowers Pacific Division AAAS Annual Meeting, 2018 | 8 | 2018 |
| Determining products of inertia for small scale UAVs JS Lorenzetti, L Bañuelos, R Clarke, OJ Murillo, A Bowers 55th AIAA Aerospace Sciences Meeting, 0547, 2017 | 7 | 2017 |
| Multiaxis Thrust Vectoring Using Axisymmetric Nozzles and Postexit Vanes on an F AH Bowers, GK Noffz, SB Grafton, ML Mason, LR Peron A-18 Configuration Vehicle, NASA TM-101741, 1991 | 7 | 1991 |
| Experimental Flight Validation of the Prandtl 1933 Bell Spanload AH Bowers, OJ Murillo, DE Berger, VS Hawkins, LJ Newton, AG Waddell, ... | 6 | 2021 |
| An Overview of an Experimental Demonstration Aerotow Program JE Murray National Aeronautics and Space Administration, Dryden Flight Research Center, 1998 | 6 | 1998 |
| Imaging supersonic aircraft shock waves LM Weinstein, K Stacy, GJ Vieira, EA Haering Jr, AH Bowers Journal of Flow Visualization and Image Processing 4 (3), 1997 | 6 | 1997 |
| Parameter estimation for the NASA F/A-18 HARV at high angles of attack M Napolitano, A Paris, J Spagnuolo, A Bowers 19th Atmospheric Flight Mechanics Conference, 3504, 1994 | 6 | 1994 |
Joseph LorenzettiStanford UniversityVerified email at stanford.edu
