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TESTS OF A 16 RELATED AIRFOILS AT HIGH SPEEDS.

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BookPublisher: Naca, Washington 1934Description: 23.DDC classification: NACA | 492

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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 492 (Browse shelf)	Not for loan		TR13342

Total holds: 0

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Previous	NACA 488 HEAT TRANSFER FROM FINNED METAL CYLINDERS IN AN AIR STREAM.	NACA 489 AIR CONDITIONS CLOSE TO THE GROUND AND THE EFFECT ON AIRPLANE LANDINGS.	NACA 491 VIBRATIONS RESPONSE OF AIRPLANE STRUCTURES.	NACA 492 TESTS OF A 16 RELATED AIRFOILS AT HIGH SPEEDS.	NACA 493 THE PHYSICAL EFFECTS OF DETONATION IN A CLOSED CYLINDRICAL CHAMBER.	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.	Next

Bond With Naca-481-491,493-500.

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