Call Number (LC) Title Results
Y 3.N 21/5:11/A19 An experimental investigation of the effect of propellers used as aerodynamic brakes on stability and control / 1
Y 3.N 21/5:11/A2 Tests of an attack-type airplane in the Ames 40- by 80-foot wind tunnel to improve the high-speed maneuvering control-force characterstics / 1
Y 3.N 21/5:11/A20 An investigation of the characteristics of alcohol-distribution tubes used for ice protection on aircraft windshields / 1
Y 3.N 21/5:11/A21 An additional investigation of the high-speed lateral-control characteristics of spoilers / 1
Y 3.N 21/5:11/A22 An investigation of a thermal ice-prevention system for a C-46 cargo airplane. : 4 - Results of flight tests in dry-air and natural-icing conditions / 1
Y 3.N 21/5:11/A23 Flight tests of the thermal ice-prevention equipment on the B-17F airplane / 1
Y 3.N 21/5:11/A24 An investigation of 0.15-chord ailerons on a low-drag tapered wing at high speeds / 1
Y 3.N 21/5:11/A25 An investigation of a thermal ice-prevention system for a C-46 cargo airplane. : 2 - The design, construction, and preliminary tests of the exhaust-air heat exchanger / 1
Y 3.N 21/5:11/A26 A comparison of analytically and experimentally determined isothermal pressure losses in a heat-exchanger installation / 1
Y 3.N 21/5:11/A27 An experimental investigation of the thrust and torque produced by propellers used as aerodynamic brakes / 1
Y 3.N 21/5:11/A28 Measurements in flight of the stability, lateral control, and stalling characteristics of an airplane equipped with full-span zap flaps and spoiler-type ailerons / 1
Y 3.N 21/5:11/A29 Flight tests of several exhaust-gas-to-air heat exchangers in a B-17F airplane / 1
Y 3.N 21/5:11/A3 Tests of a thermal ice-prevention system for a wing leading-edge landing-light installation / 1
Y 3.N 21/5:11/A30 Effect of the performance of a turbosupercharged engine of an exhaust-gas-to-air heat exchanger for thermal ice prevention / 1
Y 3.N 21/5:11/A31 Wind-tunnel investigation of the effect of jet-motor operation on stability / 1
Y 3.N 21/5:11/A32 Measurements in flight of the lateral-control characteristics of an airplane equipped with full-span zap flaps and simple circular-arc-type aiilerons / 1
Y 3.N 21/5:11/A33 An investigation of a thermal ice-prevention system for a C-46 cargo airplane. : 6 - Dry-air performance of thermal system at several twin- and single-engine operating conditions at various altitudes / 1
Y 3.N 21/5:11/A34 Preliminary investigation and design of an air-heated wing for Lockheed 12 airplane / 1
Y 3.N 21/5:11/A35 Development of thermal ice-prevention equipment for the B-24D airplane / 1
Y 3.N 21/5:11/A37 A comparison of two flight-test procedures for the determination of aileron control capabilities of an airplane / 1