Modified double-slit interferometer for shock-wave investigations.

"This work was carried out as part of Project SQUID which is supported by the Office of Naval Research under Contract Nonr-1858 (25)."

Plasma studies in a shock tube,

"This work was supported by the Air Research and Development Center, Griffis Air Force Base, New York."

A graphical solution of shock equations

Contract no. AF 18(603)-141.

Radiation pressure confinement, the shock pinch and feasibility of fusion propulsion,

Caption title.

A study of finite-difference methods as applied to hypersonic viscous shock-layer equations

"Contract no. Nonr 2653(00)."

Test time in low pressure shock tubes.

"SSD-TDR-62-204. Report no TDR-169 (3230-12)TN-5."

Shock tube driver techniques and attenuation measurements,

"Contract AF 18(603)-10, Mechanics Division, Air Force Office of Scientific Research, ARDC, Washington."

Low-density research in the hypersonic shock tunnel

"The experimental study reported here has been performed under the sponsorship of the Fluid Dynamics Branch, Aeronautical Research laboratories of the U.S. Air Force Air Research and Development Command, Contract no. AF 33(616)-6025."

48-inch hypersonic shock tunnel; description and capabilities.

Mode of access: Internet.

Normal shock wave parameters in equilibrium air,

Mode of access: Internet.

Normal shock waves in air: equilibrium composition and flow parameters for velocities from 26,000 to 50,000 ft/sec.

"Contract no. NASr-119."

Shock-tube measurements of transition probabilities for oxygen and nitric oxide,

Mode of access: Internet.

Annotated bibliography on shock,

"Prepared under the auspices of the Committee on Shock, Division of Medical Sciences, National Academy of Sciences-National Research Council."

Table and charts of equilibrium normal-shock and shock-tube properties for pure carbon dioxide with velocities from 1 to 16 km/sec /

Chiefly tables.

Factors affecting thermal shock resistance of polyphase ceramic bodies

Mode of access: Internet.