Call Number (LC) Title Results
Y 3.N 21/5:9/202 The Late⁺ѓcoe⁺ђre 521 "Lieutenant de vaisseau Paris" commercial flying boat (French), A Two-deck Six-engine semicantilever sesquiplane. 1
Y 3.N 21/5:9/203 Vickers-Supermarine "Scapa" (British), A military flying boat. 1
Y 3.N 21/5:9/204 Short "Empire" commercial flying boat (British), An all-metal cantilever monoplane. 1
Y 3.N 21/5:9/205 The Hafner A. R. III gyroplane (British) 1
Y 3.N 21/5:9/206 Aircraft Circulars : Armstrong Whitworth 27 "Ensign" commercial airplane (British), An all-metal high-wing monoplane. 1
Y 3.N 21/5:9/207 Baynes Bee light airplane (British), A two-seat high-wing monoplane. 1
Y 3.N 21/5:9/208 The Airspeed "Oxford" training airplane (British), A two-engine cantilever monoplane. 1
Y 3.N 21/5:9/209 Fairey "Battle" medium bomber airplane (British), An all-metal low℗--wing cantilever monoplane. 1
Y 3.N 21/5:11/ Wartime reports / 1
Y 3.N 21/5:11/A.8 Kinetic temperature of wet surfaces : a method of calculating the amount of alcohol required to prevent ice, and the derivation of the psychometric equation / 1
Y 3.N 21/5:11/A1 Investigation of slipstream effects on a wing-inlet oil-cooler ducting system of a twin-engine airplane in the Ames 40- by 80-foot wing tunnel / 1
Y 3.N 21/5:11/A10 Analysis of the thermal ice-prevention system for wing leading-edge landing-light installations / 1
Y 3.N 21/5:11/A11 Computation of hinge-moment characteristics of horizontal tails from section data / 1
Y 3.N 21/5:11/A12 The effect of wall interference upon the aerodynamic characteristics of an airfoil spanning a closed-throat circular wind tunnel / 1
Y 3.N 21/5:11/A13 Measurements in flight of the pressure distribution on the right wing of a P-39N-1 airplane at several values of Mach power / 1
Y 3.N 21/5:11/A14 Tunnel-wall corrections to rolling and yawing moments due to aileron deflection in closed rectangular wind tunnels / 1
Y 3.N 21/5:11/A15 Measurement of free water in cloud under conditions of icing / 1
Y 3.N 21/5:11/A16 An investigation of a thermal ice-prevention system for a C-46 cargo airplane. : 3 - Description of thermal ice-prevention equipment for wings, empennage, and windshield / 1
Y 3.N 21/5:11/A17 An analytical investigation of a thermal-electric means of preventing ice formations on a propeller blade / 1
Y 3.N 21/5:11/A18 Wind-tunnel investigation of ailerons on a low-drag airfoil. : 3 - The effect of tabs / 1