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COMPUTATION OF THE TWO-DIMENSIONAL, FLOW IN A LAMINAR BOUNDARY LAYER.

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BookPublisher: Naca, Washington 1934Description: 11.DDC classification: NACA | 497

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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 497 (Browse shelf)	Not for loan		TR13347

Total holds: 0

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Previous	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.	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	Next

Bound With Naca-481-496,498-500.

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