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AERODYNAMIC DERIVATIVES WITH RESPECT TO SIDESLIP FOR A DELTA WING WITH SMALL DIHEDRAL AT SUPERSONIC SPEEDS

By: Hunter-Tod, J.H.

Contributor(s): Robinson,A.

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BookSeries: College Of Aeronautics Coa No 12. Publisher: DDC classification: R-12

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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	R-12 (Browse shelf)	Not for loan		TR3037

Total holds: 0

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Previous	Q CR-1248 COMPUTER MECHANIZATION OF REENTRY QUATIONS WITH FOUR DEGREES OF FREEDOM.	R, -3269 CONCEPT OF COMPLEX STIFFNESS APPLIED TO PROBLEMS OF OSCILLETIONS WITH VISCOUS AND HYSTERATIC DAMPLING	R, -3674 APPROXIMATE ANALYSIS OF THE NON-LINNAR LATRAL MOTION OF A SLENDER AIRCRAFT (HP-115) AT LOW SPEEDS	R-12 AERODYNAMIC DERIVATIVES WITH RESPECT TO SIDESLIP FOR A DELTA WING WITH SMALL DIHEDRAL AT SUPERSONIC SPEEDS	R-202 DEVELOPMENTS IN UNDERSTANDING THE BEHAVIOUR AND DESIGN OF SLAB- COLUMN CONNECTIONS	R-207 SURFACE SETTLEMENT OF A DEEP ELASTIC STRATUM WHOSE MODULUS IN CREASES LIMEARLY WITH DEPTH	R-23 Some notes on the performance of small high speed wind tunnels	Next

Bound With: Coa Rep 12-30

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