| The Dynamics of Low Initial Disturbance Turbulent Jets RE Drubka, P Reisenthel, HM Nagib Physics of Fluids A: Fluid Dynamics (1989-1993) 1 (10), 1723-1735, 1989 | 55 | 1989 |
| Development of a Nonlinear Indicial Model for Maneuvering Fighter Aircraft PH Reisenthel 34th Aerospace Sciences Meeting and Exhibit (AIAA 96-0896), 1996 | 53 | 1996 |
| Seeding of Helical Modes in the Initial Region of an Axisymmetric Jet SM Kusek, TC Corke, P Reisenthel Experiments in Fluids 10 (2-3), 116-124, 1990 | 42 | 1990 |
| Development of a Nonlinear Indicial Model Using Response Functions Generated by a Neural Network PH Reisenthel 35th Aerospace Sciences Meeting and Exhibit (AIAA 97-0337), 1997 | 39 | 1997 |
| On the Dynamical Scaling of Forced Unsteady Separated Flows HM Nagib, PH Reisenthel, DJ Koga AIAA Shear Flow Control Conference (AIAA-85-0553), 1985 | 30 | 1985 |
| Volterra Kernel Extrapolation for Modeling Nonlinear Aeroelastic Systems at Novel Flight Conditions RJ Prazenica, PH Reisenthel, AJ Kurdila, MJ Brenner Journal of Aircraft 44 (1), 149-162, 2007 | 29 | 2007 |
| Prediction of Unsteady Aerodynamic Forces Via Nonlinear Kernel Identification PH Reisenthel Presented at CEAS/AIAA/ICASE/NASA Langley International Forum on …, 1999 | 27 | 1999 |
| The Scaling and Control of Vortex Geometry Behind Pitching Cylinders R Montividas, P Reisenthel, H Nagib 2nd Shear Flow Conference (AIAA 89-1003), 1989 | 26 | 1989 |
| Control of Separated Flowfields Using Forced Unsteadiness DJ Koga, P Reisenthel, HM Nagib Illinois Institute of Technology, 1984 | 23 | 1984 |
| Application of Multifidelity Expected Improvement Algorithms to Aeroelastic Design Optimization PH Reisenthel, TT Allen 10th AIAA Multidisciplinary Design Optimization Conference, AIAA SciTech …, 2014 | 22 | 2014 |
| Data-Based Aerodynamic Modeling Using Nonlinear Indicial Theory PH Reisenthel, MT Bettencourt 37th Aerospace Sciences Meeting and Exhibit (AIAA 99-0763), 1999 | 22 | 1999 |
| Control of Separated Flows Using Forced Unsteadiness PH Reisenthel, HM Nagib, DJ Koga AIAA Shear Flow Control Conference (AIAA 85-0556), 1985 | 22 | 1985 |
| Application of Nonlinear Indicial Modeling to the Prediction of a Dynamically Stalling Wing PH Reisenthel 14th Applied Aerodynamics Conference (AIAA 96-2493), 1996 | 21 | 1996 |
| A Practical Approach for Calculating Aerodynamic Indicial Functions with a Navier-Stokes Solver DJ Lesieutre, PH Reisenthel, MFE Dillenius 32nd Aerospace Sciences Meeting and Exhibit (AIAA 94-0059), 1994 | 21 | 1994 |
| A Nonlinear Indicial Prediction Tool for Unsteady Aerodynamic Modeling PH Reisenthel, MT Bettencourt, JH Myatt, DS Grismer 23rd Atmospheric Flight Mechanics Conference (AIAA 98-4350), 1998 | 20 | 1998 |
| Extraction of Nonlinear Indicial and Critical State Responses from Experimental Data PH Reisenthel, MT Bettencourt 37th Aerospace Sciences Meeting and Exhibit (AIAA 99-0764), 1999 | 16 | 1999 |
| Innovative Fusion of Experiment and Analysis for Missile Design and Flight Simulation PH Reisenthel, JF Love, DJ Lesieutre, MFE Dillenius NATO-RTO Symposium on Innovative Missile Systems, Amsterdam, The Netherlands …, 2006 | 14 | 2006 |
| Hybrid Instability in an Axisymmetric Jet with Enhanced Feedback PH Reisenthel Illinois Institute of Technology, 1988 | 14 | 1988 |
| Control of Two and Three Dimensional Modes in the Initial Region of an Axisymmetric Jet SM Kusek, TC Corke, P Reisenthel 2nd Shear Flow Conference (AIAA 89-968), 1989 | 13 | 1989 |
| Volterra Kernel Identification and Extrapolation for the F/A-18 Active Aeroelastic Wing RJ Prazenica, PH Reisenthel, AJ Kurdila, MJ Brenner Proceedings of the 45th AIAA/ASME/ASCE/AHS/ASC structures, structural …, 2004 | 11 | 2004 |
John EkaterinarisProf aerospace Eng Embry riddle Bestätigte E-Mail-Adresse bei erau.edu
