Effect of simulated bearing coolant injection on the performance of a two-stage, velocity-compounded turbopump drive turbine /
by Roy G. Stabe, John F. Kline, and Edward H. Gibbs.

Description

Main Author: Stabe, Roy G.
Related Names: Gibbs, Edward H.
Kline, John F.
Lewis Research Center.
Language(s): English
Published: Washington, D.C. : National Aeronautics and Space Administration ; 1967.
Subjects: Two stage turbines.
Turbojet engines.
Turbines.
Turbine pumps.
Propulsion system performance.
Injection.
Coolants.
Note: "NASA TM X-1364."
"Lewis Research Center, Cleveland, Ohio."
"April 1967"--Cover.
Also available online from the NASA Technical Reports Server (http://ntrs.nasa.gov/). Address as of 8/03/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19670013511_1967013511.pdf.
Physical Description: 15 p. : ill. ; 27 cm.
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