Call Number (LC) Title Results
Y 3.N 21/5:6/2330 Water-landing investigation of a model having heavy beam loadings and 0 degree angle of dead rise / 1
Y 3.N 21/5:6/2331 Wind-tunnel investigation of a number of total-pressure tubes at high angles of attack. : Subsonic speeds / 1
Y 3.N 21/5:6/2332 Analysis of the effects of wing interference on the tail contributions to the rolling derivatives / 1
Y 3.N 21/5:6/2333 Transient aerodynamic behavior of an airfoil due to different arbitrary modes of nonstationary motions in a supersonic flow / 1
Y 3.N 21/5:6/2334 On reflection of shock waves from boundary layers / 1
Y 3.N 21/5:6/2335 A plan-form parameter for correlating certain aerodynamic characteristics of swept wings / 1
Y 3.N 21/5:6/2336 Some theoretical characteristics of trapezoidal wings in supersonic flow and a comparison of several wing-flap combinations / 1
Y 3.N 21/5:6/2337 Approximate calculation of turbulent boundary-layer development in compressible flow / 1
Y 3.N 21/5:6/2338 Experimental investigation of localized regions of laminar-boundary-layer separation / 1
Y 3.N 21/5:6/2339 Transonic flow past a wedge profile with detached bow wave : General analytical method and final calculated results / 1
Y 3.N 21/5:6/2340 A survey of methods for determining stability parameters of an airplane from dynamic flight measurements / 1
Y 3.N 21/5:6/2341 A least squares curve fitting method with applications to the calculation of stability coefficients from transient-response data / 1
Y 3.N 21/5:6/2342 Evaluation of packed distillation columns. 1
Y 3.N 21/5:6/2343 Comparison of theoretical and experimental response of a single-mode elastic system in hydrodynamic impact / 1
Y 3.N 21/5:6/2344 Method for calculating downwash field due to lifting surfaces at subsonic and supersonic speeds / 1
Y 3.N 21/5:6/2345 The effect of an arbitrary surface-temperature variation along a flat plate on the convective heat transfer in an incompressible turbulent boundary layer / 1
Y 3.N 21/5:6/2346 An iterative transformation procedure for numerical solution of flutter and similar characteristic-value problems / 1
Y 3.N 21/5:6/2347 Effect of aspect ratio and sweepback on the low-speed lateral control characteristics of untapered low-aspect-ratio wings equipped with retractable ailerons / 1
Y 3.N 21/5:6/2348 Effect of aspect ratio on the low-speed lateral control characteristics of unswept untapered low-aspect-ratio wings / 1
Y 3.N 21/5:6/2349 Fluctuations in a spray formed by two impinging jets / 1