Add to ORKGProgram computes specific power output, specific fuel consumption, and cycle efficiency for power systems having any number os shafts up to maximum of five. Maximum temperatures should be no higher than about 2000 K (3140 F) because molecular dissociation is not included in stoichiometry
"NASA TM X-1339.""Lewis Research Center, Cleveland, Ohio.""January 1967"--Cover.Includes bibliograph...
Three-volume publication covers theoretical, design, and performance aspects of turbines. Volumes co...
Computer program calculates the inviscid axisymmetric nozzle expansion of propellant systems having ...
Fortran 7094 computer program for calculation of design point performance of turbojet and turbofan e...
Includes errata sheet.Prepared at Lewis Research Center.Cover title.Includes bibliographical referen...
Computer program subroutines provide the thermodynamic and transport properties of hydrogen in tabul...
Program uses component performance maps to enable user to do analytical engine cycle calculations. E...
A combined thermochemical cycle analysis computer program was designed. Input to the combined progra...
Computer code was developed for calculating chemical quantities and qualities in equilibrium
Computer program calculates thermodynamic properties from basic spectroscopic data. Program capacity...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.Bi...
Computer program obtains the real-gas isentropic flow functions and thermodynamic properties of gase...
Ten energy conversion systems are defined and analyzed in terms of efficiency. These include: open-...
The Air Force and NASA share a common interest in developing advanced propulsion systems for commerc...
A general computer program for chemical equilibrium and rocket performance calculations was written ...
"NASA TM X-1339.""Lewis Research Center, Cleveland, Ohio.""January 1967"--Cover.Includes bibliograph...
Three-volume publication covers theoretical, design, and performance aspects of turbines. Volumes co...
Computer program calculates the inviscid axisymmetric nozzle expansion of propellant systems having ...
Fortran 7094 computer program for calculation of design point performance of turbojet and turbofan e...
Includes errata sheet.Prepared at Lewis Research Center.Cover title.Includes bibliographical referen...
Computer program subroutines provide the thermodynamic and transport properties of hydrogen in tabul...
Program uses component performance maps to enable user to do analytical engine cycle calculations. E...
A combined thermochemical cycle analysis computer program was designed. Input to the combined progra...
Computer code was developed for calculating chemical quantities and qualities in equilibrium
Computer program calculates thermodynamic properties from basic spectroscopic data. Program capacity...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.Bi...
Computer program obtains the real-gas isentropic flow functions and thermodynamic properties of gase...
Ten energy conversion systems are defined and analyzed in terms of efficiency. These include: open-...
The Air Force and NASA share a common interest in developing advanced propulsion systems for commerc...
A general computer program for chemical equilibrium and rocket performance calculations was written ...
"NASA TM X-1339.""Lewis Research Center, Cleveland, Ohio.""January 1967"--Cover.Includes bibliograph...
Three-volume publication covers theoretical, design, and performance aspects of turbines. Volumes co...
Computer program calculates the inviscid axisymmetric nozzle expansion of propellant systems having ...