Kooperativer Bibliotheksverbund

UID:

Format: Online-Ressource (643 p) , illustrations, tables

Edition: Online-Ausg. Chester, Vt NewsBank, inc 2007 U.S. Congressional Serial Set, 1817-1980

Series Statement: United States congressional serial set serial set no. 10318

Note: 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 , 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 , A photographic study of combustion and knock in a spark-ignition engine, by A.M. Rothrock and R.C. Spencer [No. 622], p. 213 , A study of the torque equilibrium of an auto-giro rotor, by F.J. Bailey, Jr. [No. 623], p. 235 , 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 , 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 , Appendix, p. 130 , Approximate stress analysis of multistringer beams with shear deformation of the flanges, by Paul Kuhn [No. 636], p. 469 , Auto-ignition and combustion of diesel fuel in a constant-volume bomb, by Robert F. Selden [No. 617], p. 147 , 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 , Column strength of tubes elastically restrained against rotation at the ends, by William R. Osgood [No. 615], p. 101 , 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 , Compressible flow about symmetrical Jonkowski profiles, by Carl Kaplan [No. 621], p. 197 , 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 , Drag of cylinders of simple shapes, by W.F. Lindsey [No. 619], p. 169 , Heat-transfer processes in air-cooled engine cylinders, by Benjamin Pinkel [No. 612], p. 49 , Interrelation of exhaust-gas constituents, by Harold C. Gerrish and Fred Voss [No. 616], p. 139 , List of technical reports, p. III , On sonic reciprocal relations in the theory of nonstationary flows, by I.E. Garrick [No. 629], p. 347 , Pressure distribution over airfoils with Fowler flaps, by Carl J. Wenzinger and Walter B. Anderson [No. 620], p. 177 , 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 , 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 , 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 , The aerodynamic characteristics of four full-scale propellers having different plan forms, by Edwin P. Hartman and David Biermann [No. 643], p. 617 , 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 , The crinkling strength and the bending strength of round aircraft tubing, by William R. Osgood [No. 632], p. 387 , 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 , The experimental and calculated characteristics of 22 tapered wings, by Raymond F. Anderson [No. 627], p. 273 , 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 , 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 , 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 , The transition phase in the take-off of an airplane, by J.W. Wetmore [No. 626], p. 261 , The variation with Reynolds number of pressure distribution over an airfoil section, by Robert M. Pinkerton [No. 613], p. 65 , 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 , Two dimensional subsonic compressible flow past elliptical cylinders, by Carl Kaplan [No. 624], p. 245 , © 2008 by NewsBank, Inc. All rights reserved

Language: English

URL: Volltext  (Deutschlandweit zugänglich)

UID:

Format: Online-Ressource (750 p) , illustrations, tables

Edition: Online-Ausg. Chester, Vt NewsBank, inc 2007 U.S. Congressional Serial Set, 1817-1980

Series Statement: United States congressional serial set serial set no. 10174

Note: A study of two-control operation of an airplane, by Robert T. Jones [No. 579], p. 73 , A theory of primary failure of straight centrally loaded columns, by Eugene E. Lundquist and Claude M. Fligg [No. 582], p. 141 , Air propellers in yaw, by E.P. Lesley, George F. Worley, and Stanley Moy [No. 597], p. 459 , Airfoil section characteristics as affected by variations of the Reynolds number, by Eastman N. Jacobs and Albert Sherman [No. 586], p. 227 , Alternating-current equipment for the measurement of fluctuations of air speed in turbulent flow, by W.C. Mock, Jr. [No. 598], p. 475 , An analysis of lateral stability in power-off flight with charts for use in design, by Charles H. Zimmerman [No. 589], p. 297 , An analysis of the factors that determine the periodic twist of an autogiro rotor blade, with a comparison of predicted and measured results, by John B. Wheatley [No. 600], p. 503 , An analytical and experimental study of the effect of periodic blade twist on the thrust torque, and flapping motion of an autogiro rotor, by John B. Wheatley [No. 591], p. 353 , Appendix, p. 159 , Blower cooling of finned cylinders, by Oscar W. Schey and Herman H. Ellerbrock, Jr. [No. 587], p. 269 , Characteristics of six propellers including the high-speed range, by Theodore Theodorsen, George W. Stickle, and M.J. Brevoort [No. 594], p. 401 , Cooling of airplane engine at low air speeds, by Theodore Theodorsen, M.J. Brevoort, and George W. Stickle [No. 593], p. 391 , Cooling test of a single-row radial engine with several N.A.C.A. cowlings, by M.J. Brevoort, George W. Stickle, and Herman H. Ellerbrock, Jr. [No. 596], p. 449 , Electrical thermometers for aircraft, by John B. Peterson and S.H.J. Womack [No. 606], p. 633 , Experimental investigation of wind-tunnel interference on the down wash behind an airfoil, by Abe Silverstein and S. Katzoff [No. 609], p. 689 , Flight measurements of the dynamic longitudinal stability of several airplanes and a correlation of the measurements with pilots' observations of handling characteristics, by Hartley A. Soule [No. 578], p. 69 , Flight tests of the drag and torque of the propeller in terminal-velocity dives, by Richard V. Rhode and Henry A. Pearson [No. 599], p. 493 , Fuel spray and flame formation in a compression-ignition engine employing airflow, by A.M. Rothrock and C.D. Waldron [No. 588], p. 281 , Full-scale tests of N.A.C.A. cowlings, by Theodore Theodorsen, M.J. Brevoort, and George W. Stickle [No. 592], p. 361 , Full-scale tests of a new type N.A.C.A. nose-slot cowling, by Theodore Theodorsen, M.J. Brevoort, George W. Stickle, and M.N. Gough [No. 595], p. 439 , Heat transfer to fuel sprays injected into heated gases, by Robert F. Selden and Robert C. Spencer [No. 580], p. 91 , Measurements of intensity and scale of wind-tunnel turbulence and their relation to the critical Reynolds number of spheres, by Hugh L. Dryden, G.B. Schubauer, W.C. Mock, Jr., and H.K. Skramstad [No. 581], p. 109 , Prechamber compression-ignition engine performance, by Charles S. Moore and John H. Collins, Jr. [No. 577], p. 49 , Pressure distribution measurements of an 0-2H airplane in flight, by H.A. Pearson [No. 590], p. 319 , Pressure-distribution measurements at large angles of pitch on fins of different span-chord ratio on a 1/40 scale model of the U.S. airship "Akron," by James G. McHugh [No. 604], p. 585 , Resume and analysis of N.A.C.A. lateral control research, by Fred E. Weick and Robert T. Jones [No. 605], p. 605 , Span load distribution for tapered wings with partial-span flaps, by H.A. Pearson [No. 585], p. 209 , Spinning characteristics of the XN2Y-1 airplane obtained from the spinning balance and compared with results from the spinning tunnel and from flight tests, by M.J. Bamber and R.O. House [No. 607], p. 649 , Strength of welded aircraft joints, by W.C. Brueggeman [No. 584], p. 177 , Stress analysis of beams with shear deformation of the flanges, by Paul Kuhn [No. 608], p. 669 , Table of contents, p. III , Tests of related forward-camber airfoils in the variable-density wind tunnel, by Eastman N. Jacobs, Robert M. Pinkerton, and Harry Greenberg [No. 610], p. 697 , The rolling friction of several airplane wheels and tires and the effect of rolling friction on take-off, by J.W. Wetmore [No. 583], p. 169 , Torsion tests of tubes, by Ambrose H. Stang, Walter Ramberg, and Goldie Back [No. 601], p. 515 , Wind-tunnel and flight tests of slot-lip ailerons, by Joseph A. Shortal [No. 563], p. 537 , Wind-tunnel investigation of tapered wings with ordinary ailerons and partial-span split flaps, by Carl J. Wenzinger [No. 611], p. 733 , Wind-tunnel investigation of wings with ordinary ailerons and full-span external airfoil flaps, by Robert C. Platt and Joseph A. Shortal [No. 603], p. 563 , © 2008 by NewsBank, Inc. All rights reserved

Language: English

URL: Volltext  (Deutschlandweit zugänglich)

UID:

Format: Online-Ressource (634 p) , illustrations, tables

Edition: Online-Ausg. Chester, Vt NewsBank, inc 2007 U.S. Congressional Serial Set, 1817-1980

Series Statement: United States congressional serial set serial set no. 10018

Note: A comparison of fuel sprays from several types of injection nozzles, by Dana W. Lee [No. 520], p. 251 , A flight investigation of the spinning of the F4B-2 biplane with various loads and tail surfaces, by N.F. Scudder and Oscar Seidman [No. 529], p. 413 , A turbulence indicator utilizing the diffusion of heat, by G.B. Schubauer [No. 524], p. 337 , Aerodynamic characteristics of a wing with fowler flaps, including flap loads downwash, and calculated effect of take-off, by Robert C. Platt [No. 534], p. 477 , Aerodynamic characteristics of wings with cambered external-airfoil flaps, including lateral control with a full-span flap, by Robert C. Platt [No. 541], p. 609 , Air flow in a separating laminar boundary layer, by G.B. Schubauer [No. 527], p. 369 , Altitude-pressure tables based on the United States Standard Atmosphere, by W.G. Brombacher [No. 538], p. 531 , An analysis of longitudinal stability in power-off flight with charts for use in design, by Charles H. Zimmerman [No. 521], p. 289 , Analysis of 2-spar cantilever wings with special reference to torsion and load transference, by Paul Kuhn [No. 508], p. 45 , Appendices, p. 64 , Appendix, p. 201 , Appendix, p. 249 , Appendix, p. 318 , Appendix, p. 487 , Appendix, p. 76 , Characteristics of the N.A.C.A. 23012 airfoil from tests in the full-scale and variable-density tunnels, by Eastman N. Jacobs and William C. Clay [No. 530], p. 435 , Distribution and regularity of injection from a multicylinder fuel-injection pump, by A.M. Rothrock and E.T. Marsh [No. 533], p. 465 , Experimental investigation of the Robinson-type cup anemometer, by M.J. Brevoort and U.T. Joyner [No. 513], p. 143 , Flight investigation of lateral control devices for use with full-span flaps, by H.A. Soule and W.H. McAvoy [No. 517], p. 209 , Full-scale wind-tunnel tests of a PCA-2 autogiro rotor, by John B. Wheatley and Manley J. Hood [No. 515], p. 179 , General equations for the stress analysis of rings, by Eugene E. Lundquist and Walter F. Burke [No. 509], p. 69 , Hydrogen as an auxiliary fuel in compression-ignition engines, by Harold C. Gerrish and Hampton H. Foster [No. 535], p. 495 , Interference of wing and fuselage from tests of 209 combinations in the N.A.C.A. variable-density tunnel, by Eastman N. Jacobs and Kenneth E. Ward [No. 540], p. 571 , Investigation of full-scale split trailing-edge wing flaps with various chords and hinge locations, by Rudolf Wallace [No. 539], p. 545 , List of technical reports, p. III , Noise from two-blade propellers, by E.Z. Stowell and A.F. Deming [No. 526], p. 359 , Potential flow about elongated bodies of revolution, by Carl Kaplan [516], p. 189 , Reduction of hinge moments of airplane control surfaces by tabs, by Thomas A. Harris [No. 528], p. 381 , Some effects of injection advance angle, engine-jacket temperature, and speed on combustion in a compression-ignition engine, by A.M. Rothrock and C.D. Waldron [No. 525], p. 343 , Some factors affecting combustion in an internal-combustion engine, by A.M. Rothrock and Mildred Cohn [No. 512], p. 125 , Spinning characteristics of wings. I. -- Rectangular Clark Y monoplane wing, by M.J. Bamber and C.H. Zimmerman [No. 519], p. 231 , Tests in a variable-density wind tunnel of related airfoils having the maximum camber unusually far forward, by Eastman N. Jacobs and Robert M. Pinkerton [No. 537], p. 521 , The drag of airplane wheels, wheel fairings and landing gears. II. -- Nonretractable and partly retractable landing gears, by David Biermann and William H. Herrnstein, Jr. [No. 518], p. 219 , The drag of airplane wheels, wheel fairings, and landing gears -- III, by William H. Herrnstein, Jr. and David Biermann [No. 522], p. 321 , The effect of baffles on the temperature distribution and heat-transfer coefficients of finned cylinders, by Oscar W. Schey and Vern G. Rollin [No. 511], p. 111 , The effect of water vapor on flame velocity in equivalent CO-O2 mixtures, by Ernest F. Fiock and H. Kendall King [No. 531], p. 445 , The influence of wing setting on the wing lead and rotor speed of a PCA-2 autogiro as determined in flight, by John B. Wheatley [No. 323], p. 333 , The measurements of the field of view from airplane cockpits, by Melvin N. Gough [No. 514], p. 167 , The soap-bubble method of studying the combustion of mixtures of CO and O2, by Ernest F. Fiock and Carl H. Roeder [No. 532], p. 451 , Wind-tunnel research comparing lateral control devices particularly at high angles of attack. XIII. -- Auxiliary airfoils used as external ailerons, by Fred E. Weick and Richard W. Noyes [No. 510], p. 79 , Wind-tunnel tests of a 10-foot-diameter gyroplane rotor, by John B. Wheatley and Carlton Bioletti [No. 536], p. 511 , © 2007 by NewsBank, Inc. All rights reserved

Language: English

URL: Volltext  (Deutschlandweit zugänglich)