Development of a shock-tube driven molecular beam. Contract no. AF 49(638)-793, Mechanics Division, Air Force Office of Scientific Research, Air Research and Development Command, Washington, D. C.

"AFOSR 166."

Interferometric measurement in a shock tube of dissociation rates for air and its component gases.

At head of title: Cornell University, Graduate School of Aeronautical Engineering.

Theory of electron driven shock waves

"STL/TR-60-0000-GR310."

Single-pulse shock tube studies of the kinetics of the reaction N + O [arrow right over arrow left (reversible reaction)] 2 NO between 2000-3000⁰ K,

At head of title: Combustion Dynamics Division, Air Force Office of Scientific Research, ARDC, Washington, D. C., File no. AF 18(600)-1332.

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."