Views of prominent places in Charleston, South Carolina, U.S.A., illustrating the effects of the earthquake shock, August 31st, 1886, and a sketch of the occurrence ...

Disbound Original Held in Oak Street Library Facility.

Numerical solution of plane viscous shock reflections /

Vita.

Stability of a system of equations describing the flow behind a shock /

"This work has been supported by the National Science Foundation under Grant G-1221"

Deep underground shock measurements /

"Issuance Date: May 24, 1965"--cover ; "December 1964"--title page

Clinical shock; a study of the biochemical response to injury in man.

"DA-49-193-MD-2229."

Shock induced transitions. final report /

"PNE-112F(Pt. II); Nuclear Explosions and peaceful applications."

Close-in shock studies : final report /

"PNE-104F Nuclear Explosions-Peaceful Applications."

Close-in shock studies : preliminary report /

"U.S. Atomic Energy Commission Plowshare Program ; Project Gnome, Carlsbad, New Mexico, December 10, 1961"--Cover.

Shock induced transitions, final report /

"Issued: June 28, 1963"--Cover ; "February 1, 1963"--Title page.

Shock induced transitions.

At head of title on cover: "U.S. Atomic Energy Commission Plowshare Program, Project GNOME, Carlsbad, New Mexio, December 10, 1961."

On the uniqueness of solutions for passage of shock waves through ducts of variable cross section.

"Sponsored by Project SQUID which is supported by the Office of Naval Research under Contract Nonr-1858(25), NR-098-038."

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.