Normal view MARC view ISBD view

EFFECT OF FINITE SPAN ON THE AIRLOAD DISTRIBUTIONS FOR OSCILILATING WINGS.

Material type: materialTypeLabel

BookPublisher: Nasa, Washington, D.C. 1947Description: 95.DDC classification: NACA | TN 1195

average rating: 0.0 (0 votes)

Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NACA TN 1195 (Browse shelf)	Not for loan		TR15721

Total holds: 0

Previous								Next
Previous	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	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	Next

Bound With Naca Tn-1190-1195,1196-1199.Lack Nos-1196,1197,1199

There are no comments for this item.

PKK Library