Normal view MARC view ISBD view

FLIGHT AND WIND-TUNNEL TESTS ON AN AERODYNAMICALLY COMPENSATED PILOT-STATIC HEAD FOR THE BAC 221 AIRCRAFT.

Material type: materialTypeLabel

BookPublisher: Her Majesty'S Stationery Office, London 1971Description: 28.DDC classification: ARC | C.P. 1167

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. 1167 (Browse shelf)	Not for loan		TR11173

Total holds: 0

Previous								Next
Previous	ARC C.P. 1164 BOUNDARY-LAYER PREDICTION METHODS APPLIED TO COOLING PROBLEMS IN THE GAS TURBINE.	ARC C.P. 1165 PILOTED SIMULATOR INVESTIGATIONS OF FLIGHT NEAR ZERO RATE OF CLIMB SPEED.	ARC C.P. 1166 SOME FULL-SCALE MEASUREMENTS OF THE FLOW IN THE WAKE OF A HANGAR.	ARC C.P. 1167 FLIGHT AND WIND-TUNNEL TESTS ON AN AERODYNAMICALLY COMPENSATED PILOT-STATIC HEAD FOR THE BAC 221 AIRCRAFT.	ARC C.P. 1168 BRIEF FLIGHT TESTS OF CROSSWIND LANDINGS AND SIDESTEP MANOEUVRES ON THE BAC 221 AIRCRAFT.	ARC C.P. 1169 THEORETICAL ASSESSMENT OF A METHOD FOR THE FLIGHT MEASUREMENTS OF NET ENGINE THRUST USING TOWED DRAG DEVICES.	ARC C.P. 1170 RESULTS OF A SERIES OF WIND TUNNEL MODEL BREAKDOWN TESTS ON THE TRIDENT 1 AIRCRAFT AND A COMPARISON WITH DRAG ESTIMATES AND FULL SCALE FLIGHT DATA.	Next

Bound With Arc C.P. 1161-66, 1168-70.

There are no comments for this item.

PKK Library