HEAT TRANSFER TO COMPRESSIBLE FLUIDS FLOWING IN TUBES AT SUPERSONIC VELOCITIES.
Rept. no. 2,
MASSACHUSETTS INST OF TECH CAMBRIDGE
Pagination or Media Count:
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.
- Fluid Mechanics