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WIND-TUNNEL RESEARCH COMPARING LATERAL CONTROL DEVICES,PARATICULARY AT HIGH ANGLES OF ATTACK.

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BookPublisher: Naca, Washington 1934Description: 17.DDC classification: NACA | 499

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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	NACA 499 (Browse shelf)	Not for loan		TR13349

Total holds: 0

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Previous	NACA 495 GENERAL THEORY OF AERODYNAMIC INSTABILITY AND THE MECHANISM OF FLUTTER.	NACA 497 COMPUTATION OF THE TWO-DIMENSIONAL, FLOW IN A LAMINAR BOUNDARY LAYER.	NACA 498 IMPROVED AIRPLANE WINDSHIELDS TO PROVIDE VISION IN STORARY WEATHER	NACA 499 WIND-TUNNEL RESEARCH COMPARING LATERAL CONTROL DEVICES,PARATICULARY AT HIGH ANGLES OF ATTACK.	NACA 500 THE INFLUENCE OF TIP SHAPE ON THE WING LOAD DISTRIBUTION AS DETERMIND BY FLYIGHT TESTS	NACA RM-L53A07 COMPRESSIBLE-FLOW SOLUTIONS FOR THE ACTUATOR DISK	NACA RM-L55H31 A THEORETICAL ANALYSIS OF A SIMPLE AERODYNAMIC DEVICE TO IMPROVE THE LONGITUDINAL DAMPING OF A CRUIFORM MISSILE CONFIGURATION AT SUPERSONIC SPEEDS	Next

Bound With Naca-481-498,500.

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