Call Number (LC) Title Results
Y 3.N 21/5:11/A39 A description of the Ju 88 airplane anti-icing equipment / 1
Y 3.N 21/5:11/A4 A flight investigation of the ice-prevention requirements of the United States Naval K-Type airship / 1
Y 3.N 21/5:11/A40 A method for determining the rate of heat transfer from a wing or streamline body / 1
Y 3.N 21/5:11/A42 Compressible potential flow with circulation about a circular cylinder / 1
Y 3.N 21/5:11/A43 A comparison of the effects of four-blade dual- and single-rotation propellers on the stability and control characteristics of a high-powered single-engine airplane / 1
Y 3.N 21/5:11/A45 A flight investigation of the thermal properties of an exhaust heated wing de-icing system on a Lockheed 12-A airplane / 1
Y 3.N 21/5:11/A46 Flight tests of several exhaust-gas-to-air heat exchangers / 1
Y 3.N 21/5:11/A47 Tests of thermal-electric de-icing equipment for propellers / 1
Y 3.N 21/5:11/A48 An investigation of a thermal ice-prevention system for a C-46 cargo airplane. : 7 - Effect of the thermal system on the wing-structure stresses as established in flight / 1
Y 3.N 21/5:11/A49 Flight tests of thermal ice-prevention equipment on a Lockheed 12A airplane / 1
Y 3.N 21/5:11/A5 Effect of Mach and Reynolds numbers on the maximum lift coefficient obtainable in gradual and abrupt stalls of a pursuit airplane equipped with a low-drag wing / 1
Y 3.N 21/5:11/A50 An investigation of the characteristics of a propeller alcohol feed ring / 1
Y 3.N 21/5:11/A51 Development of thermal ice-prevention equipment for the B-17F airplane / 1
Y 3.N 21/5:11/A52 An investigation of a thermal ice-prevention system for a C-46 cargo airplane. : 1 - Analysis of the thermal design for wings, empennage, and windshield / 1
Y 3.N 21/5:11/A53 Preliminary report on flight tests of an airplane having exhaust-heated wings / 1
Y 3.N 21/5:11/A54 Wind-tunnel investigation of ailerons on a low-drag airfoil. : 2 - The effect of thickened and beveled trailing edges / 1
Y 3.N 21/5:11/A55 Wind-tunnel investigation of ailerons on a low-drag airfoil. : 1 - The effect of aileron profile / 1
Y 3.n 21/5:11/A56 Thermodynamic design of double-panel, air-heated windshields for ice prevention / 1
Y 3.N 21/5:11/A57 Comparison of the energy method with the accelerometer method of computing drag coefficients from flight data / 1
Y 3.N 21/5:11/A58 Observations of the improvement in vision brought about by the application of a rain-repellent lacquer on an airplane windshield / 1