Normal view MARC view ISBD view

MEASUREMENTS OF TWO-DIMENSIONAL DERIVATIVES ON A WING-AILERON-TAB SYSTEM WITH A 1541 SECTION AEROFOIL. PART II-DIRECT TAB AND CROSS AILERON-TAB DERIVATIVES.

Material type: materialTypeLabel

BookPublisher: Her Majesty'S Stationery Office, London 1958Description: 28.DDC classification: ARC | R&M 3029

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 3029 (Browse shelf)	Not for loan Untraceable		TR11125

Total holds: 0

Previous								Next
Previous	ARC R&M 3024 MEASUREMENTS OF THE EFFECT OF WINDSCREEN SHAPES ON THE DRAG OF COCKPIT CANOPIES AT TRANSONIC AND LOW SUPERSONIC SPEEDS USING THE FREE-FLIGHT-MODEL TECHNIQUE.	ARC R&M 3025 FLIGHT EXPERIMENTS ON BOUNDARY-LAYER CONTROL FOR LOW DRAG.	ARC R&M 3027 AN INVESTIGATION OF THE VELOCITY DISTRIBUTION AROUND THE NOSE OF THE AEROFOIL WITH A FLAP.	ARC R&M 3029 MEASUREMENTS OF TWO-DIMENSIONAL DERIVATIVES ON A WING-AILERON-TAB SYSTEM WITH A 1541 SECTION AEROFOIL. PART II-DIRECT TAB AND CROSS AILERON-TAB DERIVATIVES.	ARC R&M 3032 THE EFFECTS OF TAPER ON THE SUPERVELOCITIES ON THREE-DIMENSIONAL WINGS AT ZERO INCIDENCE.	ARC R&M 3033 A SURVEY AND CORRELATION OF DATA ON HEAT TRANSFER BY FORCED CONVECTION AT SUPERSONIC SPEEDS.	ARC R&M 3035 THE ESTIMATION OF SHOCK PRESSURE RECOVERY AND EXTERNAL DRAG CONICAL CENTRE-BODY INTAKES AT SUPERSONIC SPEEDS.	Next

Bound With Arc R&M 3020-27,3032-39 Lack No. 3022,26,28,30,31,34,37

There are no comments for this item.

PKK Library