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AERODYNAMIC CHARACTERISTICS IN THE APPROACH, SUPERFINE AND NEGATIVE PITCH RANGES OF TWO FOUR-BLADED PROPELLERS WITH N.A.C.A. SERIES 16 BLADE SECTIONS

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BookPublisher: Her Majesty'S Stationery Office,London 1957Description: 23.DDC classification: ARC | R&M 3105

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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	ARC R&M 3105 (Browse shelf)	Not for loan Untraceable		TR16715

Total holds: 0

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Previous	ARC R&M 3102 CALCULATION OF THE LOAD DISTRIBUTION OVER A WING WITH ARBITRARY CAMBER AND TWIST AT SONIC SPEED	ARC R&M 3103 ASPECT-RATIO EFFECTS ON COMPRESSOR CASCADE BLADE FLUTTER	ARC R&M 3104 LONGITUDINAL STABILITY AND CONTROL OF THE SINGLE-ROTOR HELICOPTER	ARC R&M 3105 AERODYNAMIC CHARACTERISTICS IN THE APPROACH, SUPERFINE AND NEGATIVE PITCH RANGES OF TWO FOUR-BLADED PROPELLERS WITH N.A.C.A. SERIES 16 BLADE SECTIONS	ARC R&M 3122 THE FORMATION OF REGIONS OF SEPARATED FLOW ON WING SURFACES PART I LOW-SPEED TESTS ON A TWO-DIMENSIONAL UNSWEPT WING WITH A IO PER CENT THICK RAE 101 SECTION, PART II LAMINAR-SEPARATION BUBBLES AND...	ARC R&M 3123 AN APPROXIMATE METHOD OF CALCULATING THE LAMINAR BOUNDARY LAYER IN TWO-DIMENSIONAL INCOMPRESSIBLE FLOW	ARC R&M 3124 APPROXIMATE CALCULATIONS OF THE LAMINAR BOUNDARY LAYER WITH SUCTION, WITH PARTICULAR REFERENCE TO THE SUCTION REQUIREMENTS FOR BOUNDARY-LAYER STABILITY ON AEROFOILS OF DIFFERENT THICKNESS/CHORD RATIOS	Next

Bound With Arc R&M3101-04,3106-20

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