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Title: Prediction of induced rolling moments in slender cruciform canard controlled configurations at moderately high angles of attack.
Author: Gnanasekaran, V.
Awarding Body: Queen's University
Current Institution: Queen's University Belfast
Date of Award: 1981
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No abstract available
Supervisor: Not available Sponsor: Not available
Qualification Name: Thesis (Ph.D.) Qualification Level: Doctoral
EThOS ID:  DOI: Not available
Keywords: Missile aerodynamic design