Longitudinal stability characteristics and damping in pitch of detla Wings

Object/Artifact

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AVRO Museum

Name/Title

Longitudinal stability characteristics and damping in pitch of detla Wings

Entry/Object ID

687

Description

McCarter's Thesis for The College of Aeronautics at Cranfield - Longitudinal stability of 45 and 60 degree sweep angles (Delta wing) are addressed in subsonic, transonic and supersonic speeds.

Category

Thesis

Web Links and URLs

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General Notes

Note

Date / Time Period: 1954-Jul Pages: 40 Author / Artist: W.B. McCarter Publisher: The College of Aeronautics Cranfield