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CALCULATION OF DERIVATIVES FOR A CROPPED DELTA WING WITH AN OSCILLATING CONSTANT-CHORD FLAP IN A SUPERSONIC AIR STREAM

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BookPublisher: Her Majesty'S Stationery Office,London 1958Description: 34.DDC classification: - | -

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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	- - (Browse shelf)	Not for loan Untraceable		TR892

Total holds: 0

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Previous	620 EN33 ENGINEERING FUNDAMENTALS AND PROBLEMS SOLVING	624.1762 SE45B SEISMIC STRONG MOTION SYNTHETICS	574.1925 D878 BIOORGANIC CHEMISTRY	- - CALCULATION OF DERIVATIVES FOR A CROPPED DELTA WING WITH AN OSCILLATING CONSTANT-CHORD FLAP IN A SUPERSONIC AIR STREAM	\ X-448 INVESTIGATION OF THE CHARACTERISTICS OF 6-FOOT DROGUE-STABILIZATION RIBBON PARACHUTES AT HIGH ALTITUDES AND LOW SUPERSONIC SPEEDS	0 - A	001 B289h The house of intellect	Next

Bound With Hmso-R&M-3050-69

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