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Aircraft gas-turbine engines: Noise reduction and vibration control. (Latest citations from Information Services in Mechanical Engineering data base). Published Search

Technical Report ·
OSTI ID:5031063
The bibliography contains citations concerning the design and analysis of aircraft gas turbine engines with respect to noise and vibration control. Included are studies regarding the measurement and reduction of noise at its source, within the aircraft, and on the ground. Inlet, nozzle and core aerodynamic studies are cited. Propfan, turbofan, turboprop engines, and applications in short take-off and landing (STOL) aircraft are included. (Contains a minimum of 202 citations and includes a subject term index and title list.)
Research Organization:
NERAC, Inc., Tolland, CT (United States)
OSTI ID:
5031063
Report Number(s):
PB-92-855600/XAB
Country of Publication:
United States
Language:
English