Trajectory Simulation of Ice Shed From a Business Jet Bombardier Aerospace, Learjet Division

Format:

Conference/Event

Author/Creator:

Chandrasekharan, Reuben, author.

Conference Name:

World Aviation Congress & Exposition (2003-09-08 : Montreal, Canada)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 2003

Summary:

Trajectories of ice shed from two variants of a business jet were computed to show that a change in fuselage length did not increase the risk of ice ingestion by the engine. A droplet trajectory code modified for solid ice shapes, was used in the analysis. This method could help reduce icing flight tests when minor modifications are made to an aircraft

Notes:

Vendor supplied data

Publisher Number:

2003-01-3032

Access Restriction:

Restricted for use by site license