1-16 of 16 Books
Design and operating features of the N.P.L. 6 in. shock tunnel
Design and operating features of the N.P.L. 6 in. shock tunnel
By L. Pennelegion
Performance estimates for a reflected-shock tunnel with a modified driver to produce high test-section Reynolds
Performance estimates for a reflected-shock tunnel with a modified driver to produce high test-section Reynolds
By James G. Woodley
The interaction of the reflected shock with the boundary layer in a shock tube and its influence on the duration of hot flow in the reflected-shock tunnel
The interaction of the reflected shock with the boundary layer in a shock tube and its influence on the duration of hot flow in the reflected-shock tunnel
By L. Davies
A theoretical analysis of the driver-reservoir method of driving hypersonic shock tunnels
A theoretical analysis of the driver-reservoir method of driving hypersonic shock tunnels
By Robert Finch Flagg
Feasibility of a high performance aerodynamic impulse facility
Feasibility of a high performance aerodynamic impulse facility
By R. L. Leonard
Shock tunnel studies of scramjet phenomena
Shock tunnel studies of scramjet phenomena
By
Numerical and analytical study of the inlet startup process in a shock tunnel environment
Numerical and analytical study of the inlet startup process in a shock tunnel environment
By H. L. Atkins
Initial operation of the UTA shock tunnel
Initial operation of the UTA shock tunnel
By Frank K. Lu
Simulation of transient flow in a shock tunnel and a high Mach number nozzle
Simulation of transient flow in a shock tunnel and a high Mach number nozzle
By P. A. Jacobs
Reactivation and upgrade of the NASA Ames 16-inch shock tunnel
Reactivation and upgrade of the NASA Ames 16-inch shock tunnel
By Daniel W. Bogdanoff
The G-Range Impulse Facility, a high-performance free-piston shock tunnel
The G-Range Impulse Facility, a high-performance free-piston shock tunnel
By J. R. Maus
Studies on an inert gas disk hall generator driven in a shock tunnel
Studies on an inert gas disk hall generator driven in a shock tunnel
By J. F Louis
Hypersonic flows about a 25 ̊sharp cone
Hypersonic flows about a 25 ̊sharp cone
By James N. Moss
Mach 4 and Mach 8 axisymmetric nozzles for a shock tunnel
Mach 4 and Mach 8 axisymmetric nozzles for a shock tunnel
By P. A. Jacobs
Studying hypersonic flight in the shock tunnel
Studying hypersonic flight in the shock tunnel
By Abraham Hertzberg
Performance data of the new free-piston shock tunnel at GALCIT
Performance data of the new free-piston shock tunnel at GALCIT
By H. G. Hornung