K. Chadwick

Plasma and flowfield induced effects on hypervelocity re-entry vehicles for L-band irradiation at near broadside aspect angles

D. Boyer, K. Chadwick, S. Andre, 1996 .

Studies of laminar, transitional, and turbulent hypersonic flows over curved compression surfaces

Michael Holden, M. Holden, Kenneth Chadwick, 1995 .

Measurements of Gas Temperature and Velocity in Hypervelocity Flows Using Diode-Laser Sensors

Ronald K. Hanson, Douglas S. Baer, Shawn Wehe, 1998 .

Measurements of boundary layer transition on cones at angle of attack for Mach numbers from 11 to 13

Michael Holden, M. Holden, Kenneth Chadwick, 1995 .

Direct Measurements of Skin Friction in Supersonic Combustion Flow Fields

J. Schetz, K. Chadwick, D. DeTurris, 1992 .

Technique for direct measurement of skin friction in high enthalpy impulsive scramjet flowfields

Rodney D. W. Bowersox, Joseph A. Schetz, Ken Chadwick, 1995 .

An actively cooled floating element skin friction balance for direct measurement in high enthalpy supersonic flows

Kenneth Michael Chadwick, K. Chadwick, 1992 .