Accession Number : AD0493871

Title :   HEAT TRANSFER TO COMPRESSIBLE FLUIDS FLOWING IN TUBES AT SUPERSONIC VELOCITIES.

Descriptive Note : Rept. no. 2,

Corporate Author : MASSACHUSETTS INST OF TECH CAMBRIDGE

Personal Author(s) : Klingensmith, K. K. ; Junge, R. M.

Report Date : 01 FEB 1947

Pagination or Media Count : 3

Abstract : The design of a recovery factor apparatus for a Mach number of 2.5 has been completed. The component parts, all of which have been fabricated, are now being assembled. The design of each of these parts is briefly discussed, as each is encountered in tracing the path of the airstream through the apparatus.

Descriptors :   (*COMPRESSIBLE FLOW, HEAT TRANSFER), GAS FLOW, SUPERSONIC FLOW, HEAT EXCHANGERS, PIPES.

Subject Categories : Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE