Search

Advanced search

Normal view MARC view ISBD view

FLIGHT DETERMINATION OF THE RUDDER POWER AND DIRECTIONAL STABILITY OF THE FAIREY DELTA 2 AIRCRAFT USING A WINGTIP PARACHUTE

By: Ingle,G.

Material type: materialTypeLabel

materialTypeLabel

BookSeries: Aeronautical Research Council Current Papers Cp No.1298. Publisher: Her Majestys Stationery Office, London 1974Description: 21.DDC classification: TR | CP-1298

average rating: 0.0 (0 votes)

Holdings ( 1 )
Title notes
Comments ( 0 )

Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	TR CP-1298 (Browse shelf)	Not for loan		TR3325

Total holds: 0

Browsing PK Kelkar Library, IIT Kanpur Shelves , Collection code: General Stacks Close shelf browser

Previous								Next
Previous	TR CP-1291 MEASUREMENT OF THE ITERNAL PERFORMANCE OF A RECTANGULAR AIR INTAKE MOUNTED ON A FUSELAGE AT MACH NUMBERS FROM 1.6 TO 2	TR CP-1293 LOW-SPEED WIND-TUNNEL TESTS ON THE LIFT-DEPENDENT DRAG OF DELTA WINGS WITH CONICAL CAMBER	TR CP-1297 VARIABILITY OF FATIGUE DAMAGE FROM FLIGHT TO FLIGHT	TR CP-1298 FLIGHT DETERMINATION OF THE RUDDER POWER AND DIRECTIONAL STABILITY OF THE FAIREY DELTA 2 AIRCRAFT USING A WINGTIP PARACHUTE	TR CP-1299 FLIGHT SIMULATION OF A WESSEX HELICOPTER A VALIDATION EXERCISE	TR CP-1300 LIST OF CURRENT PAPERS	TR CP-1321 CHARACTERISTICS OF A FAMILY OF ROOFLAP AEROFOILS DESIGNED AT THEIR DRAG-RISE CONDITION IN VISCOUS, COMPRESSIBLE FLOW	Next

Bound With: Arc Cp No.1291-1300

There are no comments for this item.

Log in to your account to post a comment.

Powered by Koha