Normal view MARC view ISBD view

MEASUREMENTS OF DIRECT PITCHING OSCILLATION DERIVATIVES FOR THREE CROPPED DELTA AND THREE ARROWHEAD PLANFORMS AT SUBSONIC AND TRANSONIC SPEEDS.

Material type: materialTypeLabel

BookPublisher: Her Majesty'S Stationery Office, London 1965Description: 30.DDC classification: ARC | R&M 3397

average rating: 0.0 (0 votes)

Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	ARC R&M 3397 (Browse shelf)	Not for loan		TR10746

Total holds: 0

Previous								Next
Previous	ARC R&M 3392 ON THE AXIAL COMPRESSION OF LONG, SLIGHTLY CURVED PANELS.	ARC R&M 3393 BOUNDARY-LAYER DRAG OF BI-CONVEX WING SECTION WITH HEAT TRANSFER AT SUPERSONIC SPEEDS.	ARC R&M 3395 UPWASH INTERFERENCE ON WINGS OF FINITE SPAN IN A RECTANGULAR WIND TUNNEL WITH CLOSED SIDE WALLS AND POROUS-SLOTTED FLOOR AND ROOF.	ARC R&M 3397 MEASUREMENTS OF DIRECT PITCHING OSCILLATION DERIVATIVES FOR THREE CROPPED DELTA AND THREE ARROWHEAD PLANFORMS AT SUBSONIC AND TRANSONIC SPEEDS.	ARC R&M 3398 THE CHANGE IN SHOCK-TUNNEL TAILORING MACH NUMBER DUE TO DRIVER GAS MIXTURES OF HELIUM AND NITROGEN.	ARC R&M 3399 NOTES AND COMMENTS ON SOME PARTICULAR FEATURES OF WIND-TUNNEL DESIGN FOLLOWING MEASUREMENTS OF FLOW DISTRIBUTION, WALL PRESSURES. IN THE N.P.L. 7FT (LOW TURBULENCE) WIND TUNNEL.	ARC R&M 3403 A WIND-TUNNEL INVESTIGATION OF THE DIRECTIONAL AND LONGITUDINAL STABILITY OF THE JAVELIN AIRCRAFT AT TRANSONIC SPEEDS, INCLUDING COMPARISON WITH FLIGHT TEST RESULTS	Next

Bound With Arc R&M3381-95, 3398-99 Lack No.3387, 3390-91, 3394 And 3396

There are no comments for this item.

PKK Library