K. C. Hendershot

发表

Some Observations on Exhaust Recirculation from Clustered Rocket Nozzles

K. C. Hendershot, 1966 .

A new approach for evaluating the performance and base environment characteristics of nonconventional rocket propulsion systems.

K. C. Hendershot, R. J. Sergeant, H. B. Wilson, 1967 .

Applications of a tube wind tunnel in supersonic testing.

K. C. Hendershot, H. B. Wilson, W. J. Sheeran, 1969 .

Results of the NASA/MSFC FA-23 plume technology test program performed in the NASA/Ames unitary wind tunnels

K. C. Hendershot, 1977 .

A perforated-wall nozzle for variable Mach number testing.

K. C. Hendershot, J. F. Martin, W. J. Sheeran, 1968 .

1/30 SCALE XSM-65A MISSILE BASE RECIRCULATION MODEL TESTS,

K. C. Hendershot, P. P. Leo, 1958 .

An evaluation of rocket plume impingement effects on the Manned Orbital Workshop

K. C. Hendershot, D. Andrews, J. A. Llinas, 1969 .

A tube wind-tunnel technique for rocket propulsion testing

K. C. Hendershot, W. J. Sheeran, 1970 .