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TWO-DIMENSIONAL WIND-TUNNEL INVESTIGATION OF HIGH-LEFT FLAP ON AN NACA 65-210 AIRFOIL SECTION.

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BookPublisher: Nasa, Washington, D.C. 1947Description: 22.DDC classification: NACA | TN 1191

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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 1191 (Browse shelf)	Not for loan		TR15717

Total holds: 0

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Previous	NACA TM-465 DISCUSSION OF PROBLEMS RELATING TO THE SAFETY OF AVIATION.	NACA TM-470 ON IMPROVEMENT OF AIR FLOW IN WIND TUNNELS .	NACA TN 1190 WAKE MEASUREMENTS BEHIND A WING SECTION OF A FIGHTER AIRPLANES IN FAST DIVES.	NACA TN 1191 TWO-DIMENSIONAL WIND-TUNNEL INVESTIGATION OF HIGH-LEFT FLAP ON AN NACA 65-210 AIRFOIL SECTION.	NACA TN 1192 CHARTS SHOEING RELATIONS AMONG PRIMARY AERODYNAMIC VARIABLES FOR HELICOPTER-PERFORMANCE ESTIMATION	NACA TN 1195 EFFECT OF FINITE SPAN ON THE AIRLOAD DISTRIBUTIONS FOR OSCILILATING WINGS.	NACA TN 2140 THEORETICAL ANTISYMMETRIC SPAN LOADING FOR WINGS OF ARBITRARY PLAN FORM AT SUBSONIC SPEEDS	Next

Bound With Naca Tn-1190,1192-1199.Lack Nos-1196,1197,1199

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