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1
Performance of thermal mass flow meters in a variable gravitational environment /
Published 2004CONNECT
Government Document Electronic eBook -
2
Validation of high aspect ratio cooling in a 89 kN (20,000 lbf) thrust combustion chamber /
Published 1996CONNECT
Government Document Electronic eBook -
3
Pressure loss predictions of the reactor simulator subsystem at NASA Glenn Research Center /
Published 2016CONNECT
Government Document Electronic eBook -
4
Orifice mass flow calculation in NASA's W-8 single stage axial compressor facility /
Published 2018CONNECT
Government Document Electronic eBook