Normal view MARC view ISBD view

DERIVATIVE MEASUREMENTS AND FLUTTER TESTS ON A RECTANGULAR WING WITH A FULLL-SPAN CONTROL SURFACE, OSCILLATING IN MODES OF WING ROLL AND AILERON ROTATION.

Material type: materialTypeLabel

BookPublisher: Her Majesty'S Stationery Office, London 1957Description: 26.DDC classification: ARC | R&M 3010

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 3010 (Browse shelf)	Not for loan Untraceable		TR11045

Total holds: 0

Previous								Next
Previous	ARC R&M 3007 THE EFFECT OF A SPIKE PROTRUDING IN FRONT OF A BLUFF BODY AT SUPERSONIC SPEEDS.	ARC R&M 3008 VELOCITY DISTRIBUTION ON THIN TAPERED ARROWHEAD AND DELTA WINGS WITH SPANWISE CONSTANT THICKNESS RATIO AT ZERO INCIDENCE.	ARC R&M 3009 LOW-SPEED WIND-TUNNEL MEASUREMENTS OF LONGITUDINAL OSCILLATORY DERIVATIVES ON THREE WING PLAN-FORMS.	ARC R&M 3010 DERIVATIVE MEASUREMENTS AND FLUTTER TESTS ON A RECTANGULAR WING WITH A FULLL-SPAN CONTROL SURFACE, OSCILLATING IN MODES OF WING ROLL AND AILERON ROTATION.	ARC R&M 3011 THE AERODYNAMIC EFFECTS OF ASPECT RATIO AND SWEEPBACK ON WING FLUTTER.	ARC R&M 3012 SCALE EFFECTS AT HIGH SUBSONIC AND TRANSONIC SPEEDS, AND METHODS FOR FIXING BOUNDARY-LAYER TRANSITION IN MODEL EXPERIMENTS.	ARC R&M 3014 FLIGHT TESTS ON A VAMPIRE MK. 5 WITH A REDESIGNED ANTI-SNAKING RUDDER.	Next

Bound With Arc R&M 3000-3009, 3011-19 Lack No. 3003,13,15.

There are no comments for this item.

PKK Library