Serial/Series Title
2 Matching Results
Results open in a new window/tab.
Results:
1 - 2 of
2
Experimental investigation of an axial-flow compressor inlet stage operating at transonic relative inlet Mach numbers 4: stage and blade-row performance of stage with axial-discharge stators
Report presenting an investigation to determine the performance characteristics of a transonic stage designed to produce transonic inlet Mach numbers relative to a succeeding stage. Results regarding rotor performance, stator performance, and stage performance are provided.
Date:
June 28, 1954
Creator:
Sandercock, Donald M.; Lieblein, Seymour & Schwenk, Francis C.
System:
The UNT Digital Library
Two-Spool Matching Procedures and Equilibrium Characteristics of a Two-Spool Turbojet Engine
Memorandum presenting two-spool matching procedures which may be employed to analyze turbojet, turboprop, and stationary power plants. The procedures were applied to obtain the sea-level static equilibrium performance of a simple two-spool turbojet engine in which the compressor and turbine performances were based on experimental results. Results regarding engine performance at sea-level static conditions, component performance, and effect of compressor-discharge bleed are provided.
Date:
June 28, 1954
Creator:
Dugan, James F., Jr.
System:
The UNT Digital Library