Low friction hull coatings for icebreakers : phase III, technical report /

Prepared by Rensselaer Polytechnic Institute, under contract DOT-CG-61589-A.

Coefficient generator and cursor for the stereomatrix 3-D display system,

"Supported in part by contract no. Atomic Energy Commission AT(11-1)1469."

System and circuit design of the transformatrix coefficient processor and output data channel,

Vita.

Path integral calculation of the three-particle direct and exchange contributions to the pair distribution function and of the third virial coefficient for He4 gas /

Thesis--Illinois.

A method for estimating wind-wave growth and decay in shallow water with high values of bottom friction /

"October 1977."

Engineering feasibility of internal friction damping as a nondestructive evaluation technique for synthetic ropes : final report /

Includes bibliographical references.

An analysis of drag coefficient at hurricane windspeeds from a numerical simulation of dynamical water level changes in Lake Okeechobee, Florida /

"October 1975."

Calculation of wave attenuation due to friction and shoaling : an evaluation /

"October 1980."

The coefficient of thermal expansion of alpha uranium as fabricated by various methods /

"U.S. Atomic Energy Commission Contract AT(29-1)-1106."

Variational and Lagrangian thermodynamics of thermal convection-- fundamental shortcomings of the heat-transfer coefficient.

Mode of access: Internet.

Laboratory study of wave energy losses by bottom friction and percolation.

Mode of access: Internet.

Time of concentration and storage coefficient values for Illinois streams /

Mode of access: Internet.

Experimental and theoretical study of low-temperature internal friction in copper.

"Contract no. AF 18(600) 1000. File no. 10-16. AFOSR-TR-58-92. ASTIA AD 162133. Cornell University, Department of Engineering Physics."

An investigation of low temperature internal friction in metals.

"Contract no. AF 18(600) 1000. File no. 10-16. AFOSR-TR-57-69. ASTIA AD 136597. Cornell University, Department of Engineering Physics.

Skin friction, heat transfer, and pressure measurements on hypersonic inlet compression surfaces in the Mach number range 7.5 to 16.

Cornell Aeronautical Laboratory, Inc., Buffalo. Report no. AA-1948-Y-3