Call Number (LC) Title Results
Y 3.N 21/5:11/L267 Determination of towline tension and stability of spin-recovery parachutes / 1
Y 3.N 21/5:11/L268 The effect of angle of bend between plate elements on the local instability of formed Z-sections / 1
Y 3.N 21/5:11/L269 Correlation of flight data on limit pressure coefficients and their relation to high-speed burbling and critical tail loads / 1
Y 3.N 21/5:11/L27 Bending and shear stresses developed by the instantaneous arrest of the root of a cantilever beam rotating with constant angular velocity about a transverse axis through the root / 1
Y 3.N 21/5:11/L270 Analysis of effect of rolling pull-outs on wing and aileron loads of a fighter plane / 1
Y 3.N 21/5:11/L271 Additional design charts relating to the stalling of tapered wings / 1
Y 3.N 21/5:11/L272 Flight tests of F2A-2 airplane with full-span slotted flaps and trailing-edge and slot-lip ailerons / 1
Y 3.N 21/5:11/L273 Calibration of three temperature probes and a pressure probe at high speeds / 1
Y 3.N 21/5:11/L274 Effect of turbulence on air-flow measurements behind orifice plates / 1
Y 3.N 21/5:11/L275 A preliminary investigation of the characteristics of air scoops on a fuselage / 1
Y 3.N 21/5:11/L276 Requirements for satisfactory flying qualities of airplanes / 1
Y 3.N 21/5:11/L277 Aerodynamic and hydrodynamic tests of a family of models of flying-boat hulls derived from a streamline body NACA model 84 series / 1
Y 3.N 21/5:11/L278 Performance of compressor-turbine jet-propulsion systems / 1
Y 3.N 21/5:11/L279 The effect of streamlining the afterbody of an N.A.C.A. cowling / 1
Y 3.N 21/5:11/L28 Stability of a body stabilized by fins and suspended from an airplane / 1
Y 3.N 21/5:11/L280 Compression tests of six curved paper-base plastic panels with outward-acting normal pressure / 1
Y 3.N 21/5:11/L281 Limitations of lifing-line theory for estimation of aileron hinge-moment characteristics / 1
Y 3.N 21/5:11/L282 The design of the optimum hull for a large long-range flying boat / 1
Y 3.N 21/5:11/L283 Charts for helicopter-performance estimation / 1
Y 3.N 21/5:11/L284 Column and plate compressive strengths of aircraft structural materials. : Extruded 14S-T aluminum alloy / 1