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THEORETICAL ANTISYMMETRIC SPAN LOADING FOR WINGS OF ARBITRARY PLAN FORM AT SUBSONIC SPEEDS

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BookPublisher: Naca, Washington 1950Description: 95.DDC classification: NACA | TN 2140

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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 2140 (Browse shelf)	Not for loan Untraceable		TR12188

Total holds: 0

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Previous	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	NACA TN 2141 CHARTS FOR ESTIMATING DOWNWASH BEHIND RECTANGULAR TRAPEZOIDAL AND TRIANGULAR WING AT SUPERSONIC SPEEDS	NACA TN 2142 PHOTOMICROGRAPHIC INVESTIGATION OF SPONTANEOUS FREEZING TEMPERATURES OF SUPERCOLD WATER DROPLETS	NACA TN 2143 ANALYSIS OF THE EFFECTS OF BOUNDARY-LAYER CONTROL ON THE POWER-OFF LANDING PERFORMANCE CHARACTERISTICS OF A LIALSON TYPE OF AIRPLANE	Next

Bound With Naca Tn-2141-49.

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