Call Number (LC) Title Results
Y 3.N 21/5:11/L626 Langley full-scale-tunnel stability and control tests of the Bell YP-59A airplane / 1
Y 3.N 21/5:11/L627 Full-scale tunnel tests of a flying model of the Curtiss XP-55 airplane / 1
Y 3.N 21/5:11/L628 Tests of the Northrop MX-334 glider airplane in the NACA full-scale tunnel / 1
Y 3.N 21/5:11/L629 Aerodynamic tests of an NACA 66(215)-116, a = 0.6 airfoil with a 0.25c slotted flap for the Fleetwings XA-39 airplane / 1
Y 3.N 21/5:11/L63 Bending and shear stresses developed by the instantaneous arrest of the root of moving cantilever beam / 1
Y 3.N 21/5:11/L630 Full-scale tunnel measurements of the pressures on the elevator and fuselage of the Curtiss XP-55 airplane / 1
Y 3.N 21/5:11/L631 High-speed photographs of a YR-4B production rotor blade for simulated flight conditions in the Langley full-scale tunnel / 1
Y 3.N 21/5:11/L632 Cowling and cooling tests of a Fleetwings Model 33 airplane in flight / 1
Y 3.N 21/5:11/L633 Tests of a 1/40-scale wing-hull model and a 1/10-scale float-strut model of the Hughes-Kaiser cargo airplane in the two-dimensional low-turbulence pressure tunnel / 1
Y 3.N 21/5:11/L634 Characteristics of several single- and dual-rotating propellers in negative thrust / 1
Y 3.N 21/5:11/L635 Blade design data for axial-flow fans and compressors / 1
Y 3.N 21/5:11/L636 Flight tests of modifications to improve the aileron control characteristics of a North American XP-51 airplane. : (A.C. No. 41-38) / 1
Y 3.N 21/5:11/L637 Effect of a trailing-edge extension on the characteristics of a propeller section / 1
Y 3.N 21/5:11/L638 The propeller and cooling-air-flow characteristics of a twin-engine airplane model equipped with NACA Ds-type cowlings and with propellers of NACA 16-series airfoil sections / 1
Y 3.N 21/5:11/L639 Note on the interpretation of wake-survey data and its use in the estimation of induced drag due to irregularities / 1
Y 3.N 21/5:11/L64 A method for estimation of maximum stresses around a small rectangular cut-out in a sheet-string panel in shear / 1
Y 3.N 21/5:11/L640 Investigation of methods of reducing the temperature variation among cylinders on air-cooled aircraft engines / 1
Y 3.N 21/5:11/L641 Lift tests of a 0.1536c thick Douglas airfoil section of NACA 7-series type equipped with a lateral-control device for use with a full-span double-slotted flap on the C-74 airplane / 1
Y 3.N 21/5:11/L642 Stability and control tests of a 3/4-scale model of the XP-69 airplane in the NACA full-scale tunnel / 1
Y 3.N 21/5:11/L643 Airfoil section data from tests of 10 practical-construction sections of helicopter rotor blades submitted by the Sikorsky Aircraft Division, United Aircraft Corporation / 1