National Advisory Committee for Aeronautics (NACA) - 190 Matching Results

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Primary view of Tables of Coefficients for the Analysis of Stresses About Cutouts in Circular Semimonocoque Cylinders with Flexible Rings
McComb, Harvey G., Jr. & Low, Emmet F., Jr.
July 1955
Primary view of Techniques for calculating parameters of nonlinear dynamic systems from response data
Briggs, Benjamin R. & Jones, Arthur L.
July 1953
Primary view of Temperature distribution in internally heated walls of heat exchangers with noncircular flow passages using coolants with very low Prandtl number
Eckert, E. R. G. & Low, George M.
July 1951
Primary view of Temperatures, thermal stress, and shock in heat-generating plates of constant conductivity and of conductivity that varies linearly with temperature
Manson, S. V.
July 1953
Primary view of Tensile properties of 7075-T6 and 2024-T3 aluminum-alloy sheet heated at uniform temperature rates under constant load
Heimerl, George J. & Inge, John E.
July 1955
Primary view of Tensile properties of Inconel and RS-120 titanium-alloy sheet under rapid-heating and constant-temperature conditions
Heimerl, George J.; Kurg, Ivo M. & Inge, John E.
July 1956
Primary view of Theoretical aerodynamic characteristics of bodies in a free-molecule-flow field
Stalder, Jackson R. & Zurick, Vernon J.
July 1951
Primary view of Theoretical calculations of the lateral force and yawing moment due to rolling at supersonic speeds for sweptback tapered wings with streamwise tipssupersonic leading edges
Harmon, Sidney M. & Martin, John C.
July 1950
Primary view of The theoretical characteristics of triangular-tip control surfaces at supersonic speeds: Mach lines behind trailing edges
Kainer, Julian H. & King, Mary Dowd
July 1952
Primary view of Theoretical Investigation at Subsonic Speeds of the Flow Ahead of a Slender Inclined Parabolic-Arc Body of Revolution and Correlation With Experimental Data Obtained at Low Speeds
Letko, William & Danforth, Edward C. B., III
July 1954
Primary view of Theoretical investigation of longitudinal response characteristics of a swept-wing fighter airplane having a normal acceleration control system and a comparison with other types of systems
Stokes, Fred H. & Mathews, Charles W.
July 1954
Primary view of Theoretical pressure distribution and wave drags for conical boattails
Jack, John R.
July 1953
Primary view of Theoretical study of some methods for increasing the smoothness of flight through rough air
Phillips, William H. & Kraft, Christopher C., Jr.
July 1951
Primary view of Three-dimensional transonic flow theory applied to slender wings and bodies
Heaslet, Max A. & Spreiter, John R.
July 1956
Primary view of Turbulent-Heat-Transfer Measurements at a Mach Number of 3.90
Brevoort, Maurice J.
July 1956
Primary view of Unstable Convection in Vertical Channels With Heating From Below, Including Effects of Heat Sources and Frictional Heating
Ostrach, Simon
July 1955
Primary view of Vaporization rates and heat-transfer coefficients for pure liquid drops
Ingebo, Robert D.
July 1951
Primary view of Variation of Local Liquid-Water Concentration About and Ellipsoid of Fineness Ratio 5 Moving in a Droplet Field
Dorsch, Robert G. & Brun, Rinaldo J.
July 1954
Primary view of Vibration survey of four representative types of air-cooled turbine blades
Calvert, Howard F. & Smith, Gordon T.
July 1958
Primary view of Wind-tunnel investigation at low speeds of flight characteristics of a sweptback-wing jet-transport airplane model equipped with an external-flow jet-augmented slotted flap
Johnson, Joseph L., Jr.
July 1958
Primary view of Wind-tunnel investigation of effects of spoiler location, spoiler size, and fuselage nose shape on directional characteristics of a model of a tandem-rotor helicopter fuselage
Williams, James L.
July 1958
Primary view of Wind-tunnel investigation of the high-subsonic static longitudinal stability characteristics of several wing-body configurations designed for high lift-drag ratios at a Mach number of 1.4
Fournier, Paul G.
July 1958
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