An Acoustical Flight Evaluation of a Rotating Combustion Engine
An Acoustical Flight Evaluation of a Rotating Combustion Engine
- Neue Suche nach: H. R. Corwin
- Neue Suche nach: R. R. DeHoroch
- Neue Suche nach: H. R. Corwin
- Neue Suche nach: R. R. DeHoroch
Forty-six hours of flight were completed wherein the acoustical characteristics of the RC2-60 liquid-cooled Rotating Combustion Engine were evaluated. The 'Q-Star' prototype quiet aircraft was utilized as the test vehicle. It has been demonstrated that the acoustic signature of the Q-Star aircraft with the RC2-60 engine installed comes close to meeting current detectability criteria.
Dokumentinformationen
An Acoustical Flight Evaluation of a Rotating Combustion Engine
1970
46 pages
Report
Keine Angabe
Englisch
Reciprocation & Rotating Combustion Engines , Acoustics , Aircraft , Internal combustion engines , Internal combustion engine noise , Aircraft engines , Aircraft noise , Airspeed , Liquid cooled , Engine mufflers , Airplane engine noise , Flight testing , Detection , Noise analyzers , Propellers(Aerial) , Trailing edge , Performance(Engineering) , Acoustic insulation , Acoustic signatures , Qt-2 aircraft , Quiet , Q-star aircraft , Rc2-60 engines , Rotating combustion engines , Wankel engines
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