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AT LOW SPEED OF EFFECT OF SIZE AND POSITION OF CLOSED AIR DUCTS ON STATIC LONGITUDINAL AND STATIC LATERAL STABILITY CHARACTERISTICS OF UNSWEPT-MIDWING MODELS HAVING WINGS OF ASPECT RATIO 2,4, AND 6

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BookPublisher: Naca, Washington 1955Description: 45.DDC classification: NACA | TN 3481

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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 TN 3481 (Browse shelf)	Not for loan		TR13305

Total holds: 0

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Previous	NACA TN 3138 CREEP BUCKLING OF COLUNS.	NACA TN 3139 TIME-DEPENDENT BUCKLING OF A UNIFORMLY HEATED COLUMN.	NACA TN 3480 FREE-SPINNING-TUNNEL INVESTIGATION OF GYROSCOPIC EFFECTS OF JET-ENGINE ROTATING PARTS (OR OF ROTATING PROPELLERS) ON SPIN AND SPIN RECOVERY	NACA TN 3481 AT LOW SPEED OF EFFECT OF SIZE AND POSITION OF CLOSED AIR DUCTS ON STATIC LONGITUDINAL AND STATIC LATERAL STABILITY CHARACTERISTICS OF UNSWEPT-MIDWING MODELS HAVING WINGS OF ASPECT RATIO 2,4, AND 6	NACA TN 3482 SUPPLEMENTARY CHARTS FOR ESTIMATING PERFORMANCE OF HIGH-PERFORMANCE HELICOPTERS	NACA TN 3483 AN ANALYSIS OF ACCELERATION, AIRSPEED, AND GUST-VELOCITY DATA FROM A FOUR-ENGINE TRANSPORT AIRPLANE IN OPERATIONS ON AN EASTERN UNITED STATES ROUTE	NACA TN 3484 ON SPECTRAL ANALYSIS OF RUNWAY ROUGHNESS AND LOADS DEVELOPED DURING TAXIING	Next

Bound With Naca Tn 3480,3482-89

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