Call Number (LC) Title Results
Y 3.N 21/5:6/2579 Approximate methods for calculating the flow about nonlifting bodies of revolution at high high supersonic airspeeds / 1
Y 3.N 21/5:6/2580 An analysis of an x-ray absorption method for measurement of high gas temperatures / 2
Y 3.N 21/5:6/2581 Deflections of a simply supported rectangular sandwich plate subjected to transverse loads / 1
Y 3.N 21/5:6/2582 General consideration of problems in compressible flow using the hodograph method / 1
Y 3.N 21/5:6/2583 A semiempirical procedure for computing the water-pressure distribution on flat and v-bottom prismatic surfaces during impact or planing / 1
Y 3.N 21/5:6/2584 An analysis of flow in rotating passage of large radial-inlet centrifugal compressor at tip speed of 700 feet per second / 1
Y 3.N 21/5:6/2585 Calculation of aerodynamic forces on a propeller in pitch or yaw / 1
Y 3.N 21/5:6/2586 Fundamental effects of cold-work on some cobalt-chromium-nickel-iron base creep-resistant alloys / 1
Y 3.N 21/5:6/2587 Influence of wing and fuselage on the vertical-tail contribution to the low-speed rolling derivatives of midwing airplane models with 45 degree sweptback surfaces / 1
Y 3.N 21/5:6/2588 Transonic flow past a wedge profile with detached bow wave - details of analysis / 1
Y 3.N 21/5:6/2589 An analytical investigation using aerodynamic limitations of several designs of high stage pressure ratio multistage compressors / 1
Y 3.N 21/5:6/2590 Calculations on the forces and moments for an oscillating wing-aileron combination in two-dimensional potential flow at sonic speed / 1
Y 3.N 21/5:6/2591 The effects of Reynolds number on the application of NACA 16-series airfoil characteristics to propeller design / 1
Y 3.N 21/5:6/2592 Orientation of orifices on bodies of revolution for determination of stream static pressure at supersonic speeds / 1
Y 3.N 21/5:6/2593 Design of two-dimensional channels with prescribed velocity distributions along the channel walls. : 1 - Relaxation solutions / 1
Y 3.N 21/5:6/2594 Investigation of the structural damping of a full-scale airplane wing / 1
Y 3.N 21/5:6/2595 Design of two-dimensional channels with prescribed velocity distributions along the channel walls. 1
Y 3.N 21/5:6/2596 An impulse-momentum method for calculating landing-gear contact conditions in eccentric landings / 1
Y 3.N 21/5:6/2597 Investigation of laminar boundary layer in compressible fluids using the Crocco method / 1
Y 3.N 21/5:6/2598 A technique applicable to the aerodynamic design of inducer-type multistage axial-flow compressors / 1