2 Matching Results
Results open in a new window/tab.
Results:
1 - 2 of
2
Theoretical and Experimental Investigation of Additive Drag
"The significance of additive drag is discussed and equations for determining its approximate value are derived. Charts are presented giving values of additive drag for open-nose inlets and for annular-nose inlets with conical flow at the inlet. The effects of variable inlet total-pressure recovery and static pressures on the center body are investigated, and an analytical method of predicting the variation of pressure on the center body with mass-flow ratio is given" (p. 1).
Date:
May 21, 1951
Creator:
Sibulkin, Merwin
System:
The UNT Digital Library
Internal Flow and Burning Characteristics of 16-inch Ram Jet Operating in a Free Jet at Mach Numbers of 1.35 and 1.73
The effects of mass-flow ratio on the additive drag and normal-shock position of a single oblique-shock diffuser are presented. Also evaluated is the variation with operating condition of the velocity distribution at the combustion-chamber inlet. A comparison with connected-pipe data is included.
Date:
May 21, 1951
Creator:
Perchonok, Eugene & Farley, John M.
System:
The UNT Digital Library