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STUDIES IN STABILITY AND CONTROL ANALYSIS OF AIRFRAMES HAVING NONLINEAR AERODYNAMIC CHARACTERISTICS

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BookSeries: College Of Aeronautics No.171. Publisher: College Of Aeronautics, Cranfield 1966Description: 22.DDC classification: TR | COA-171

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	TR COA-171 (Browse shelf)	Not for loan		TR3069

Total holds: 0

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Previous	TR COA-169 DESIGN METHOD FOR THE DILUTION ZONES OF GAS TURBINE COMBUSTION CHAMBERS	TR COA-17 SOLUTION OF A LOAD DIFFUSION PROBLEM BY RELAXATION METHODS	TR COA-17 Study of the stress distributions necessary to maintain rubber in a state of torsion	TR COA-171 STUDIES IN STABILITY AND CONTROL ANALYSIS OF AIRFRAMES HAVING NONLINEAR AERODYNAMIC CHARACTERISTICS	TR COA-172 ADVANCED COURSE IN AIR TRANSPORT ENGINEERING	TR COA-174 COLLEGE OF AERONAUTICS WHIRLING ARM INITIAL DEVELOPMENT TESTS	TR COA-175 FREQUENCY RESPONSE OF AN AIRCRAFT AS DETERMINED FROM TRANSIENT FLIGHT TESTS USING THE FOURIER TRANSFORMATION METHOD OF ANALYSIS	Next

Bound With: Coa No. 163-178

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