Equations for the dynamic response of a closed-cycle gas turbine to changes in input parameters are developed which are readily adaptable to a digital computer. A sample step calculation is given for a typical case. (D.L.C.)
U.S. Atomic Energy Commission depository collection.
Note:
DOE contract number: AT(04-3)-187 NSA number: NSA-18-003177 OSTI Identifier 4134371 Research organization: General Atomic Div. General Dynamics Corp., San Diego, Calif.