Call Number (LC) Title Results
Y 3.N 21/5:6/3429 Static stability of fuselages having a relatively flat cross section / 1
Y 3.N 21/5:6/3430 On slender delta wings with leading-edge separation / 1
Y 3.N 21/5:6/3431 An analysis of the stability and ultimate compressive strength of short sheet-stringer panels with special reference to the influence of riveted connection between sheet and stringer / 1
Y 3.N 21/5:6/3432 Circumferential distribution of propeller-slipstream total-pressure rise at one radial station of a twin-engine transport airplane / 1
Y 3.N 21/5:6/3433 Total lift and pitching moment of thin arrowhead wings oscillating in supersonic potential flow / 1
Y 3.N 21/5:6/3434 A study of normal acceleration and operating conditions experienced by helicopters in commercial and military operations / 1
Y 3.N 21/5:6/3435 A statistical study of wing lift at ground contact for four transport airplanes / 1
Y 3.N 21/5:6/3436 An investigation of several NACA 1-series nose inlets with and without protruding central bodies at high-subsonic Mach numbers and at a Mach number of 1.2 / 1
Y 3.N 21/5:6/3437 Preliminary investigation of a submerged air scoop utilizing boundary-layer suction to obtain increased pressure recovery / 1
Y 3.N 21/5:6/3438 On the kernel function of the integral equation relating lift and downwash distributions of oscillating wings in supersonic flow / 1
Y 3.N 21/5:6/3439 Analysis of ear formation in deep-drawn cups / 1
Y 3.N 21/5:6/3440 Hovering flight tests of a four-engine-transport vertical take-off airplane model utilizing a large flap and extensible vanes for redirecting the propeller slipstream / 1
Y 3.N 21/5:6/3441 An NACA vane-type angle-of-attack indicator for use at subsonic and supersonic speeds / 1
Y 3.N 21/5:6/3442 A preliminary investigation of aerodynamic characteristics of small inclined air outlets at transonic Mach numbers / 1
Y 3.N 21/5:6/3443 Shearing effectiveness of integral stiffening / 1
Y 3.N 21/5:6/3444 Friction, wear, and surface damage of metals as affected by solid surface films / 1
Y 3.N 21/5:6/3445 Design and performance of throttle-type fuel controls for engine dynamic studies / 1
Y 3.N 21/5:6/3446 Effect of ammonia addition on limits of flame propagation for isooctane-air mixtures at reduced pressures and elevated temperatures / 1
Y 3.N 21/5:6/3447 Analytic determination of the discharge coefficients of flow nozzles / 1
Y 3.N 21/5:6/3448 Theoretical analysis of incompressible flow through a radial-inlet centrifugal impeller at various weight flows. : 1 - Solution by a matrix method and comparison with an approximate method / 1