The estimation of oscillatory wing and control derivatives
By: W.W A Acum.
Contributor(s): H C Garner.
Material type: BookPublisher: DDC classification: NATO | AGARD R-340Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
---|---|---|---|---|---|---|---|
Technical Report | PK Kelkar Library, IIT Kanpur | General Stacks | NATO AGARD R-340 (Browse shelf) | Not for loan | TR16629 |
Total holds: 0
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NATO AGARD R-337 Design aims for stability and control of piloted aircraft | NATO AGARD R-338 Design criteria for missiles | NATO AGARD R-339 State of the art of estimation of derivatives | NATO AGARD R-340 The estimation of oscillatory wing and control derivatives | NATO AGARD R-353 PITCH-YAW-ROLL COUPLING | NATO AGARD R-354 APPLICATION DU CALCULATEUR ANALOGIQUE A L'ETUDE DU COUPLAGE DES MOUVEMENTS LONGITUDINAUX ET TRANSVERSAUX D'UN AVION | NATO AGARD R-355 INFLUENCE OF DEFLECTION OF THE CONTROL SURFACES ON THE FREE-FLIGHT BEHAVIOUR OF AN AEROPLANE |
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