1966 26 p refs (NASA-TN-D-3731) CFSTI: HC $1 00/MF $0.50 CSCL 21C Noise measurements and variations of ion ... field for mercury and argon propellants agreed well with those obtained from experimental values determined from curves of ... to study the problems associated with turbines for high-temperature- engine application. was investigated experimentally ... walls were in excellent agreement with the outlet pressure distribution calculated for free-vortex outlet- flow conditionsanbsp;...
|Title||:||NASA scientific and technical reports|
|Author||:||United States. National Aeronautics and Space Administration. Scientific and Technical Information Division|