A supersonic fan equipped variable cycle engine for a Mach 2.7 supersonic transport
By: prepared for NASA Lewis Research Center.
Contributors: Lewis Research Center; Massachusetts Institute of Technology. Gas Turbine Laboratory
Publisher: Lewis Research Center
Published: 1985
Place of publication: Cleveland, Ohio
Number of pages: 107
Subjects: Supersonic transports; Turbofan engines
Notes: Bibliographical references: p.102.