author = { United States Congress Senate AND United States National Advisory Committee for Aeronautics Allen, H. Julian AND Anderson, Raymond F. AND Anderson, Walter B. AND Bailey, F.J AND Becker, John V. AND Biermann, David AND Delano, James B. AND Diehl, Walter S. AND Garrick, I.E AND Gerrish, Harold C. AND Gracey, W. AND Greenberg, Harry AND Hartman, Edwin P. AND Hootman, James A. AND Jacobs, Eastman N. AND Jones, Robert Thomas AND Kaplan, Carl AND Katzoff, S. AND Kuhn, Paul AND Rothrock, A.M AND Silverstein, Abe AND Pinkel, Benjamin AND Wenzinger, Carl J. AND Voss, Fred AND Soule, Hartley Akin AND Pearson, Henry A. AND Wetmore, Joseph W. AND Rhode, Richard V. AND Spencer, Robert C. AND Selden, Robert F. AND Pinkerton, Robert M. AND Lindsey, W.F AND Osgood, William R. },

title = { Twenty-fourth annual report of the National Advisory Committee for Aeronautics, 1938. Including technical reports Nos. 612 to 644 },

publisher = {},

year = {1939},

abstract = {A discussion of certain problems connected with the design of hulls of flying boats and the use of general test data, by Walter S. Diehl [No. 625], p. 253},

abstract = {A flight comparison of conventional ailerons on a rectangular wind and of conventional and floating wing-tip ailerons on a tapered wing, by H.A. Soule and W. Gracey [No. 630], p. 351},

abstract = {A photographic study of combustion and knock in a spark-ignition engine, by A.M. Rothrock and R.C. Spencer [No. 622], p. 213},

abstract = {A study of the torque equilibrium of an auto-giro rotor, by F.J. Bailey, Jr. [No. 623], p. 235},

abstract = {Aerodynamic characteristics of a large number of airfoils tested in the variable-density wind tunnel, by Robert M. Pinkerton and Harry Greenberg [No. 628], p. 297},

abstract = {Airfoil section characteristics as applied to the prediction of air forces and their distribution on wings, by Eastman N. Jacobs and R.V. Rhode [No. 631], p. 357},

abstract = {Appendix, p. 130},

abstract = {Approximate stress analysis of multistringer beams with shear deformation of the flanges, by Paul Kuhn [No. 636], p. 469},

abstract = {Auto-ignition and combustion of diesel fuel in a constant-volume bomb, by Robert F. Selden [No. 617], p. 147},

abstract = {Calculation of the chordwise load distribution over airfoil sections with plain, split, or serially hinged trailing-edge flaps, by H. Julian Allen [No. 634], p. 435},

abstract = {Column strength of tubes elastically restrained against rotation at the ends, by William R. Osgood [No. 615], p. 101},

abstract = {Comparative flight and full-scale wind-tunnel measurements of the maximum life of an airplane, by Abe Silverstein, S. Katzoff, and James A. Hootman [No. 618], p. 161},

abstract = {Compressible flow about symmetrical Jonkowski profiles, by Carl Kaplan [No. 621], p. 197},

abstract = {Determination of the boundary-layer transition on three symmetrical airfoils in the N.A.C.A. full-scale wind tunnel, by Abe Silverstein, and John V. Becker [No. 637], p. 491},

abstract = {Drag of cylinders of simple shapes, by W.F. Lindsey [No. 619], p. 169},

abstract = {Heat-transfer processes in air-cooled engine cylinders, by Benjamin Pinkel [No. 612], p. 49},

abstract = {Interrelation of exhaust-gas constituents, by Harold C. Gerrish and Fred Voss [No. 616], p. 139},

abstract = {List of technical reports, p. III},

abstract = {On sonic reciprocal relations in the theory of nonstationary flows, by I.E. Garrick [No. 629], p. 347},

abstract = {Pressure distribution over airfoils with Fowler flaps, by Carl J. Wenzinger and Walter B. Anderson [No. 620], p. 177},

abstract = {Pressure distribution over an N.A.C.A. 23012 airfoil with an N.A.C.A. 23012 external-airfoil flap, by Carl J. Wenzinger [No. 614], p. 85},

abstract = {Pressure distribution over an N.A.C.A. 23012 airfoil with a slotted and a plain flap, by Carl J. Wenzinger and James B. Delano [No. 633], p. 403},

abstract = {Tests of five full-scale propellers in the presence of a radical and a liquid-cooled engine nacelle, including test of two spinners, by David Biermann and Edwin P. Hartman [No. 642], p. 587},

abstract = {The aerodynamic characteristics of four full-scale propellers having different plan forms, by Edwin P. Hartman and David Biermann [No. 643], p. 617},

abstract = {The aerodynamic characteristics of full-scale propellers having 2, 3, and 4 blades of Clark Y and R.A.F 6 airfoil sections, by Edwin P. Hartman and David Biermann [No. 640], p. 547},

abstract = {The crinkling strength and the bending strength of round aircraft tubing, by William R. Osgood [No. 632], p. 387},

abstract = {The effect of compressibility on eight full-scale propellers operating in the take-off and climbing range, by David Biermann and Edwin P. Hartman [No. 639], p. 517},

abstract = {The experimental and calculated characteristics of 22 tapered wings, by Raymond F. Anderson [No. 627], p. 273},

abstract = {The influence of lateral stability on disturbed motions of an airplane with special reference to the motions produced by gusts, by Robert T. Jones [No. 638], p. 507},

abstract = {The negative thrust and torque of several full-scale propellers and their application to various flight problems, by Edwin P. Hartman and David Biermann [No. 641], p. 571},

abstract = {The torsional and bending deflection of full-scale aluminum-alloy propeller blades under normal operating conditions, by Edwin P. Hartman and David Biermann [No. 644], p. 627},

abstract = {The transition phase in the take-off of an airplane, by J.W. Wetmore [No. 626], p. 261},

abstract = {The variation with Reynolds number of pressure distribution over an airfoil section, by Robert M. Pinkerton [No. 613], p. 65},

abstract = {Theoretical stability and control characteristics of wings with various amounts of taper and twist, by Henry A. Pearson and Robert T. Jones [No. 635], p. 451},

abstract = {Two dimensional subsonic compressible flow past elliptical cylinders, by Carl Kaplan [No. 624], p. 245},

booktitle = {United States congressional serial set ; serial set no. 10318},

booktitle = {Senate document / 76th Congress, 1st session. Senate ; no. 3},

address = { Washington, DC },

url = { http://slubdd.de/katalog?TN_libero_mab2 }