1 "Wave Diagrams for Nonsteady Flows in Ducts" Inc. 56-59, 1955
2 "Theory of Two Stage Hypervelocity Launcher to Give Constant Driving Pressure at the Model" (17) : 113-125, 1963
3 "The Early Years of Aerodynamic Ranges, Light-Gas Guns, and High Velocity Impact" 17 : 151-182, 1995
4 "Optimization Study of The Ames 0.5" Two-Stage Light Gas Gun" 20 : 131-142, 1997
5 "Numerical Study of the Free-Piston Shock Tunnel Performance" tan : 313-319, 1994
6 "Nonstationary Flows and Shock Waves" oxford : 100-125, 1994
7 "Improving the Performance of Two Stage Light Gas Guns by Adding a Diaphragm in the Pump Tube" 17 : 81-92, 1995
8 "Enhanced Hypervelocity Launcher ? Capabilities to 16 Km/s" 17 : 183-194, 1995
9 "Development of High-Velocity Gas-Dynamics Gun" (5) : 183-207, 1987
10 "Design Limitations on Ultra-High Velocity Projectile Launchers" (10) : 185-196, 1990
1 "Wave Diagrams for Nonsteady Flows in Ducts" Inc. 56-59, 1955
2 "Theory of Two Stage Hypervelocity Launcher to Give Constant Driving Pressure at the Model" (17) : 113-125, 1963
3 "The Early Years of Aerodynamic Ranges, Light-Gas Guns, and High Velocity Impact" 17 : 151-182, 1995
4 "Optimization Study of The Ames 0.5" Two-Stage Light Gas Gun" 20 : 131-142, 1997
5 "Numerical Study of the Free-Piston Shock Tunnel Performance" tan : 313-319, 1994
6 "Nonstationary Flows and Shock Waves" oxford : 100-125, 1994
7 "Improving the Performance of Two Stage Light Gas Guns by Adding a Diaphragm in the Pump Tube" 17 : 81-92, 1995
8 "Enhanced Hypervelocity Launcher ? Capabilities to 16 Km/s" 17 : 183-194, 1995
9 "Development of High-Velocity Gas-Dynamics Gun" (5) : 183-207, 1987
10 "Design Limitations on Ultra-High Velocity Projectile Launchers" (10) : 185-196, 1990
11 "Constant Acceleration Flows and Applications to High Speed Guns" (11) : 1967
12 "Computational Design of Hypervelocity Launchers" 17 : 849-860, 1995
13 "Area Change with a Free Piston Shock Tube" (2) : 396-397, 1964
14 "A Two-Stage Free-Piston Driver" 9 : 239-248, 1999
15 "A Two Stage Light Gas Gun for the Study of High Speed Impact in Propellants" 2001
16 "A Study of Free Piston Shock Tunnel" (5) : 2160-2165, 1967