Performance degradation of propeller systems due to rime ice accretion

Korkan, K. D.; Dadone, L.; Shaw, R. J.

doi:10.2514/6.1982-286

20th Aerospace Sciences Meeting 1982

DOI: 10.2514/6.1982-286

|View full text |Cite

Performance degradation of propeller systems due to rime ice accretion

K. D. Korkan

L. Dadone

R. J. Shaw

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...

Citation Types

Supporting

Mentioning

Contrasting

Year Published

1983

1998

Publication Types

Select...

Other2

Relationship

Self Cite0

Independent2

Authors

Journals

Cited by 2 publications

References 0 publications

Supporting

Mentioning

Contrasting

Order By: Relevance

Three dimensional droplet trajectory code for propellers of arbitrary geometry

Farag

Bragg

1998

36th AIAA Aerospace Sciences Meeting and Exhibit

View full text Add to dashboard Cite

A three-dimensional droplet impingement code for aircraft propellers has been developed. The code allows the modeling of propellers of arbitrary geometry in three dimensions, but is limited to modeling axi-symmetric spinner / nacelles combinations. The code was used to analyze several 3-D wind tunnel propeller-nacelle models which were experimentally studied. The code was also used to validate a theoretical relationship between two-dimensional and three-dimensional impingement efficiencies for rotating propellers. The effects of the spinner, engine nacelle geometry, contraction of the slipstream, and blade-to-blade interference on the impingement efficiency and limits of impingement were studied. Parametric studies of the effects of the advance ratio J and droplet size on the efficiencies and limits were performed. NOMENCLATURE Ad Droplet's cross-sectional Area. B Buoyancy force vector. CD Droplet drag coefficient. Ci Local lift coefficient. d droplet diameter. D Drag force vector. F r Froude number of the flow.

show abstract

Three dimensional droplet trajectory code for propellers of arbitrary geometry

Farag

Bragg

1998

36th AIAA Aerospace Sciences Meeting and Exhibit

View full text Add to dashboard Cite

show abstract

Predicting Aircraft Performance Degradation Due to Ice Accretion

Bragg

Gregorek

1983

SAE Technical Paper Series

View full text Add to dashboard Cite

scite is a Brooklyn-based organization that helps researchers better discover and understand research articles through Smart Citations–citations that display the context of the citation and describe whether the article provides supporting or contrasting evidence. scite is used by students and researchers from around the world and is funded in part by the National Science Foundation and the National Institute on Drug Abuse of the National Institutes of Health.

Contact Info

customersupport@researchsolutions.com

10624 S. Eastern Ave., Ste. A-614

Henderson, NV 89052, USA

This site is protected by reCAPTCHA and the Google Privacy Policy and Terms of Service apply.

Blog Terms and Conditions API Terms Privacy Policy Contact Cookie Preferences Do Not Sell or Share My Personal Information

Made with 💙 for researchers

Part of the Research Solutions Family.

Performance degradation of propeller systems due to rime ice accretion

Cited by 2 publications

References 0 publications

Three dimensional droplet trajectory code for propellers of arbitrary geometry

Three dimensional droplet trajectory code for propellers of arbitrary geometry

Predicting Aircraft Performance Degradation Due to Ice Accretion

Contact Info

Product

Resources

About