Propulsion Systems Analysis
Noise-Reduction Benefits Analyzed for Over-the-Wing-Mounted Advanced Turbofan Engines
Integrated Supportability Analysis and Cost System Enhanced

First article

Table of contents

Last updated April 21, 2000, by Nancy.L.Obryan@nasa.gov

Responsible NASA Official: Gynelle.C.Steele@nasa.gov
216-433-8258

Point of contact for NASA Glenn's Research & Technology reports: Cynthia.L.Dreibelbis@nasa.gov
216-433-2912
SGT, Inc.

Web page curator: Nancy.L.Obryan@nasa.gov
216-433-5793
Wyle Information Systems, LLC

NASA Web Privacy Policy and Important Notices