Normal view MARC view ISBD view

SLENDER-BODY THEORY CALCULATIONS OF THE EFFECT ON LIFT AND MOMENT OF MOUNTING THE WING OFF THE FUSELAGE CENTRE-LINE.

Material type: materialTypeLabel

BookPublisher: Her Majesty'S Stationery Office, London 1965Description: 49.DDC classification: ARC | C.P. 830

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 C.P. 830 (Browse shelf)	Not for loan		TR10938

Total holds: 0

Previous								Next
Previous	ARC C.P. 827 THE TIME REQUIRED FOR HIGH SPEED AIRSTREAMS TO DISINTEGRATE WATER DROPS.	ARC C.P. 828 MEASUREMENTS OF VORTEX-BREAKDOWN POSITION AT LOW SPEED ON A SERIES OF SHARP-EDGED SYMMETRICAL MODELS.	ARC C.P. 829 A UNIFIELD THEORY OF FRICTION, HEAT TRANSFER AND MASS TRANSFER IN THE TURBULENT BOUNDARY LAYER AND WALL JET.	ARC C.P. 830 SLENDER-BODY THEORY CALCULATIONS OF THE EFFECT ON LIFT AND MOMENT OF MOUNTING THE WING OFF THE FUSELAGE CENTRE-LINE.	ARC C.P. 832 REVIEW OF GENERAL OPERATING EXPERIENCE WITH A JET-LIFT VTOL RESEARCH AIRCRAFT (SHORT S.C.I.)	ARC C.P. 833 A SURVEY OF AIRCRAFT HANDLING CRITERIA	ARC C.P. 834 AN EXPERIMENTAL CHECK ON THE THEORETICAL RELATIONSHIP BETWEEN THE SPECTRAL DENSITY AND THE PROBABILITY DISTRIBUTION OF CROSSINGS FOR A STATIONARY RANDOM PROCESS ...TURBULENT AIR.	Next

Bound With Arc C.P.821-829

There are no comments for this item.

PKK Library