These lectures address numerous engine airframe integration aspects relating to rotor wing aircraft. Various areas of engine airframe integration, including the impact of advanced engine design variables to specific propulsion subsystems, i.e. engine air inlets, are discussed. Other propulsion system integration aspects such as engine/rotor/drive system torsional stability and transient response are also addressed.
Engine-Airframe Integration for Rotorcraft
1986
152 pages
Report
No indication
English
Aircraft , Jet & Gas Turbine Engines , Rotary wing aircraft , Airframes , Symposia , Helicopter engines , Gas turbines , Integrated systems , Installation , Air intakes , Aerodynamic stability , Torsion , Transients , Compatibility , Engine air systems components , Exhaust systems , Cooling , Bleed systems , Infrared radiation , Transmission gears , Drives , Computer aided design , Finite element analysis , Composite materials , Aeronautical engineering , Manufacturing , Life cycle costs , Foreign technology , Gear drives , NATO furnished
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