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GARY T. CHAPMAN

Observed names: G. CHAPMAN, G. Chapman, G. T. Chapman, G.T. Chapman, GARY CHAPMAN, Gary Chapman, Gary T. Chapman, Gary. T. Chapman
Observed institutions: Ames Research Center, Computer Professionals for Social Responsibility, University of Florida, National Aeronautics and Space Administration, Eloret (United States), University of California, Berkeley, Stanford University
OpenAlex ID: A5111476357
A method for extracting aerodynamic coefficients from free-flight data
1970 · GARY T. CHAPMAN, DONN B. KIRK · AIAA Journal · 133
Onset of aerodynamic side forces at zero sideslip on symmetric forebodies at high angles of attack
1974 · E. KEENER, G. CHAPMAN · Mechanics and Control of Flight Conference · 112
Similarity in Vortex Asymmetries over Slender Bodies and Wings
1977 · Earl R. Keener, Gary T. Chapman · AIAA Journal · 111
Topology of Flow Separation on Three-Dimensional Bodies
1991 · Gary T. Chapman, Leslie A. Yates · Applied Mechanics Reviews · 78
Side forces on a tangent ogive forebody with a fineness ratio of 3.5 at high angles of attack and Mach numbers from 0.1 to 0.7
1977 · E. R. Keener, G. T. Chapman, et al. · University of Michigan Library Repository · 68
Nonlinear problems in flight dynamics involving aerodynamic bifurcations
1985 · Murray Tobak, G. T. Chapman · NASA Technical Reports Server (NASA) · 65
Topological classification of flow separation on three-dimensional bodies
1986 · G. CHAPMAN · 24th Aerospace Sciences Meeting · 51
Effects of Mach number and afterbody length on aerodynamic side forces at zero sideslip on symmetric bodies at high angles of attack
1976 · E. KEENER, G. CHAPMAN, et al. · 14th Aerospace Sciences Meeting · 50
Mathematical modeling of the aerodynamic characteristics in flight dynamics
1984 · Murray Tobak, G. T. Chapman, et al. · NASA Technical Reports Server (NASA) · 49
Side forces on forebodies at high angles of attack and Mach numbers from 0.1 to 0.7: two tangent ogives, paraboloid and cone
1977 · E. R. Keener, G. T. Chapman, et al. · NASA STI Repository (National Aeronautics and Space Administration) · 48
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Streamlines, vorticity lines, and vortices around three-dimensional bodies
1992 · Leslie A. Yates, Gary T. Chapman · AIAA Journal · 46
Dynamic stability testing of the Genesis Sample Return Capsule
2000 · F. Cheatwood, Gerald Winchenbach, et al. · AIAA Aerospace Sciences Meeting and Exhibit · 38
Modeling aerodynamic discontinuities and onset of chaos in flight dynamical systems
1987 · M. Tobak, G. T. Chapman, et al. · Annals of Telecommunications · 34
Dynamics of planetary probes - Design and testing issues
1998 · Gary Chapman, Leslie Yates · AIAA Aerospace Sciences Meeting and Exhibit · 27
Computers in Battle: Will They Work?
1988 · Edwin E. Salpeter, David Bellin, et al. · Computers in Physics · 22
Nonlinear problems in flight dynamics
1984 · G. T. Chapman, Murray Tobak · NASA Technical Reports Server (NASA) · 21
Observations, Theoretical Ideas, and Modeling of Turbulent Flows—Past, Present, and Future
1985 · Gary T. Chapman, Murray Tobak · Applied mathematical sciences · 20
Streamlines, vorticity lines, and vortices
1991 · LESLIE YATES, GARY CHAPMAN · AIAA Aerospace Sciences Meeting · 18
Dynamic Stability of Blunt Atmospheric Entry Configurations
2002 · Gerald L. Winchenbach, Gary T. Chapman, et al. · Journal of Spacecraft and Rockets · 17
Shock Tube as a Device for Testing Transonic Airfoils at High Reynolds Numbers
1979 · William J. Cook, Leroy L. Presley, et al. · AIAA Journal · 17
Ballistic range and aerothermodynamic testing
1991 · A. W. Strawa, G. T. Chapman, et al. · Journal of Aircraft · 16
Transonic Aerodynamics of a Lifting Orion Crew Capsule from Ballistic Range Data
2010 · Jeffrey D. Brown, David W. Bogdanoff, et al. · Journal of Spacecraft and Rockets · 15
Limit cycle analysis of planetary probes
1999 · Gary Chapman, Leslie Yates · AIAA Aerospace Sciences Meeting and Exhibit · 14
Aerodynamic ballistic range analysis using generalized math models
1996 · Leslie Yates, Gary Chapman · AIAA Atmospheric Flight Mechanics Conference · 14
A Subsonic High-Angle-of-Attack Flow Investigation at Several Reynolds Numbers
1978 · Mark H. Clarkson, Gerald N. Malcolm, et al. · AIAA Journal · 14
Works count: 108
Citation count: 1,408
H-index: 18
I10-index: 36
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