Call Number (LC) Title Results
Y 3.N 21/5:6/4182 Physical characteristics and test conditions of an ethylene-heated high-temperature jet / 1
Y 3.N 21/5:6/4183 Investigation of effects of distributed surface roughness on a turbulent boundary layer over a body of revolution at a Mach number of 2.01 / 1
Y 3.N 21/5:6/4184 Measurement of static pressure on aircraft / 1
Y 3.N 21/5:6/4185 Wind-tunnel investigation of effect of sweep on rolling derivatives at angles of attack up to 13 degrees and at high subsonic Mach numbers, including a semiempirical method of estimating the rolling derivatives / 1
Y 3.N 21/5:6/4186 Heat transfer in isotropic turbulence during the final period of decay / 1
Y 3.N 21/5:6/4187 High-speed hydrodynamic characteristics of a flat plate and 20 degree dead-rise surface in unsymmetrical planing conditions / 1
Y 3.N 21/5:6/4188 Charts relating the compressive and shear buckling stresses of longitudinally supported plates to the effective deflectional stiffness of the supports / 1
Y 3.N 21/5:6/4189 Lift and moment on thin arrowhead wings with supersonic edges oscillating in symmetric flapping and roll and application to the flutter of an all-movable control surface / 1
Y 3.N 21/5:6/4190 Experimental investigation of the lateral trim of a wing-propeller combination at angles of attack up to 90 degrees with all propellers turning in the same direction / 1
Y 3.N 21/5:6/4191 Analysis of horizontal-tail loads in pitching maneuvers on a flexible swept-wing jet bomber / 1
Y 3.N 21/5:6/4192 Three-degree-of-freedom evaluation of the longitudinal transfer functions of a supersonic canard missile configuration including changes in forward speed / 1
Y 3.N 21/5:6/4193 Subsonic flight investigation of methods to improve the damping of lateral oscillations by means of a viscous damper in the rudder system in conjuction with adjusted hinge-moment parameters / 1
Y 3.N 21/5:6/4194 Comparison of hydrodynamic-impact acceleration and response for systems with single and with multiple elastic modes / 1
Y 3.N 21/5:6/4195 Shape of initial portion of boundary of supersonic axisymmetric free jets at large jet pressure ratios / 1
Y 3.N 21/5:6/4196 A method for the calculation of the lateral response of airplanes to random turbulence / 1
Y 3.N 21/5:6/4197 Summary of flutter experiences as a guide to the preliminary design of lifting surfaces on missiles / 1
Y 3.N 21/5:6/4198 Effects of airplane flexibility on wing strains in rough air at 35,000 feet as determined by a flight investigation of a large swept-wing airplane / 1
Y 3.N 21/5:6/4199 A flight investigation of the effects of varied lateral damping on the effectiveness of a fighter airplane as a gun platform / 1
Y 3.N 21/5:6/4200 Effectiveness of boundary-layer control, obtained by blowing over a plain rear flap in combination with a forward slotted flap, in deflecting a slipstream downward for vertical take-off / 1
Y 3.N 21/5:6/4201 Collection of zero-lift drag data on bodies of revolution from free-flight investigations / 1