Tests covered range of simulated density altitudes from 4000 to 33,000 ft, of velocities between fins from Mach number of 0.05 to near sonic values, and of heat inputs from 0 to 500 Btu per hr psi of cylinder wall surface. See also Engineering Index 1947 p 34. (released 1948; 20¢)
Compressibility and heating effects on pressure loss and cooling of baffled cylinder barrel
Nat Advisory Committee Aeronautics -- Report
1944
22 pages
Bibliography
Report
English
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Engineering Index Backfile | 1946
|Cylinder barrel cooling with bonded preformed copper fins
Engineering Index Backfile | 1941
|