Prediction of Propeller Performance in Icing Conditions Using Vortex Theory-Reference-Cited by-同舟云学术

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Prediction of Propeller Performance in Icing Conditions Using Vortex Theory

Published:2009-06-14 Issue: Volume: Page:
ISSN:
Container-title:1st AIAA Atmospheric and Space Environments Conference
language:
Short-container-title:

Author:

Busch Greg¹,Bragg Michael¹,Broeren Andy²

Affiliation:

1. University of Illinois at Urbana-Champaign

2. NASA Glenn Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-4259

Reference22 articles.

1. Dumont,C.,Pellicano,P.,Smith,T.,andRiley,J."ResultsFromaFull-ScalePropellerIcingTest,"AIAAPaper 2008-0432,46thAIAAAerospaceSciencesMeeting&Exhibit,Reno,NV,Jan.2008.

2. Corson,Jr.,B.W.,andMaynard,J.D."TheEffectofSimulatedIcingonPropellerPeformance,"NACATN-1084, Jul.1946.

3. Preston,G.M.,andBlackman,C.C."EffectsofIceFormationsonAirplanePerformance,"NACATN-1598,May 1948.

4. Neel,Jr.,C.B.,andBright,L.G."TheEffectofIceFormationsonPropellerPerformance,"NACATN-2212,Oct. 1950.

5. Performance degradation of propeller systems due to rime ice accretion

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