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

Technical Report · Mon Jun 01 00:00:00 EDT 1992

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
• Resource Relation: Other Information: Updated with each order. Supersedes PB89-851760. Prepared in cooperation with Cambridge Scientific Abstracts, Washington, DC. Sponsored in part by National Technical Information Service, Springfield, VA
• Country of Publication: United States
• Language: English

Related Subjects

33 ADVANCED PROPULSION SYSTEMS
63 RADIATION, THERMAL, AND OTHER ENVIRON. POLLUTANT EFFECTS ON LIVING ORGS. AND BIOL. MAT.
AIRCRAFT
GAS TURBINE ENGINES
BIBLIOGRAPHIES
MECHANICAL VIBRATIONS
NOISE POLLUTION ABATEMENT
ACOUSTICS
AERODYNAMICS
AIRCRAFT COMPONENTS
DESIGN
EVALUATION
MITIGATION
TURBOFAN ENGINES
DOCUMENT TYPES
ENGINES
EQUIPMENT
FLUID MECHANICS
HEAT ENGINES
INTERNAL COMBUSTION ENGINES
MACHINERY
MECHANICS
POLLUTION ABATEMENT
TURBOMACHINERY
330103* - Internal Combustion Engines- Turbine
560400 - Other Environmental Pollutant Effects