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shock tunnels

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View Design and operating features of the N.P.L. 6 in. shock tunnel By L. Pennelegion

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

View Performance estimates for a reflected-shock tunnel with a modified driver to produce high test-section Reynolds By James G. Woodley

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

View 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

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

View A theoretical analysis of the driver-reservoir method of driving hypersonic shock tunnels By Robert Finch Flagg

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

View Feasibility of a high performance aerodynamic impulse facility By R. L. Leonard

Feasibility of a high performance aerodynamic impulse facility

Feasibility of a high performance aerodynamic impulse facility

By R. L. Leonard

View Shock tunnel studies of scramjet phenomena By

Shock tunnel studies of scramjet phenomena

Shock tunnel studies of scramjet phenomena

By

View Numerical and analytical study of the inlet startup process in a shock tunnel environment By H. L. Atkins

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

View Initial operation of the UTA shock tunnel By Frank K. Lu

Initial operation of the UTA shock tunnel

Initial operation of the UTA shock tunnel

By Frank K. Lu

View Simulation of transient flow in a shock tunnel and a high Mach number nozzle By P. A. Jacobs

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

View Reactivation and upgrade of the NASA Ames 16-inch shock tunnel By Daniel W. Bogdanoff

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

View The G-Range Impulse Facility, a high-performance free-piston shock tunnel By J. R. Maus

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

View Studies on an inert gas disk hall generator driven in a shock tunnel By J. F Louis

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

View Hypersonic flows about a 25 ̊sharp cone By James N. Moss

Hypersonic flows about a 25 ̊sharp cone

Hypersonic flows about a 25 ̊sharp cone

By James N. Moss

View Mach 4 and Mach 8 axisymmetric nozzles for a shock tunnel By P. A. Jacobs

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

View Studying hypersonic flight in the shock tunnel By Abraham Hertzberg

Studying hypersonic flight in the shock tunnel

Studying hypersonic flight in the shock tunnel

By Abraham Hertzberg

View Performance data of the new free-piston shock tunnel at GALCIT By H. G. Hornung

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