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WING-FUSELAGE INTERFERENCE TAIL BUFFETING, AND FLOW ABOUT THE TAIL OF A LOW-WING MONOPLANE.

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BookPublisher: Naca, Washington 1934Description: 21.DDC classification: NACA | 482

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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 482 (Browse shelf)	Not for loan		TR13332

Total holds: 0

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Previous	MISM RN-1971 STRONG MOTION RECORDS AND SIMULATION ANALYSIS OF KII BUILDING IN SAN FERNANDO EARTHQUAKE	NA D-715 AN EXPERIMENTAL INVESTIGATION OF THE DAMPING OF LIQUID OSCILLATIONS IN CYLINDRICAL TANKS WITH VARIOUS BAFFLES	NACA 1421 A THEORETICAL INVESTIGATION OF THE DRAG OF GENERALIZED AIRCRAFT CONFIGURATIONS IN SUPERSONIC FLOW.	NACA 482 WING-FUSELAGE INTERFERENCE TAIL BUFFETING, AND FLOW ABOUT THE TAIL OF A LOW-WING MONOPLANE.	NACA 483 EFFECT OF MODERATE AIR FLOW ON THE DISTRIBUTION OF FUEL SPRAYS AFTER INJECTION CUT-OFF.	NACA 484 A FLIGHT INVESTIGATION OF THE EFFECT OF MASS DISTRIBUTION AND CONTROL SETTING ON THE SPINNING OF THE XN2Y-1 AIRPLANE.	NACA 486 INFRARED RADIATION FROM EXPOLSIONS IN A SPARK-IGNATION ENGINE.	Next

Bound With Naca-481,483-500

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