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Design and evaluation of fluidized bed heat recovery for diesel engine systems

Pittsburgh, PA. : Westinghouse Electric Corp., [1985] 1985

The determination of exhaust cloud dimensions from films of space shuttle launches

Zak, R. A.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1987. 1987

Exhaust environment measurements of a turbofan engine equipped with an afterburner and 2D nozzle

Brase, L. O.
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990. 1990

Low-pressure performance of annular, high-pressure (40-atm), high-temperature, (2480 K) combustion s

Wear, Jerrold D., author.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, September 1980. 1980-

Measurements of a turbulent horseshoe vortex formed around a cylinder

Eckerle, Wayne Alan.
East Hartford, CT : United Technologies Research Center ; Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, [1986] 1986

Optical and probe determination of soot concentrations in a model gas turbine combustor

Eckerle, Wayne Alan.
East Hartford, CT : United Technologies Research Center : Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, [1986] 1986

Pulsed plasma thruster contamination

Myers, Roger Metcalf, author.
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, September 1996. 1996-

Theoretical study on the effect of the design of small (milli-newton) thruster jets on molecular con

Riley, Ben R.
Evansville, Ind. : University of Evansville, Dept. of Physics ; [Washington, D.C. : National Aeronautics and Space Administration, 1986] 1986