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Format: Online-Ressource (433 p) , illustrations, tables

Edition: Online-Ausg. Chester, Vt NewsBank, inc 2008 U.S. Congressional Serial Set, 1817-1980

Series Statement: United States congressional serial set serial set no. 10678

Note: A graphical method of determining pressure distribution in two-dimensional flow, by Robert T. Jones and Doris Cohen, N.A.C.A. [No. 722], p. 313 , A high-speed motion-picture study of normal combustion, knock, and preignition in a spark-ignition engine, by A.M. Rothrock, R.C. Spencer, and Cearcy D. Miller, N.A.C.A. [No. 704], p. 15 , A simplified theoretical method of determining the characteristics of a lifting rotor in forward flight, by F.J. Bailey, Jr., N.A.C.A. [No. 716], p. 209 , An analysis of the stability of an airplane with free controls, by Robert T. Jones and Doris Cohen, N.A.C.A. [No. 709], p. 109 , An apparatus for measuring rates of discharge of a fuel-injection system, by Francis J. Dutee, N.A.C.A. [No. 714], p. 193 , Analysis and prediction of longitudinal stability of airplanes, by R.R. Gilruth and M.D. White, N.A.C.A. [No. 711], p. 137 , Appendix, p. 118 , Determination of control-surface characteristics from NACA plain-flap and tab data, by Milton B. Ames, Jr. and Richards I. Sears, N.A.C.A. [No. 721], p. 295 , Effect of aging on mechanical properties of aluminum-alloy rivets, by Frederick C. Roop, National Bureau of Standards [No. 724], p. 353 , Effect of body nose shape on the propulsive efficiency of a propeller, by G.W. Stickle, John L. Crigler, and Irven Naiman, N.A.C.A. [No. 725], p. 371 , Flow coefficients of monosleeve valves, by C.D. Waldron, N.A.C.A. [No. 717], p. 227 , Internal-flow systems for aircraft, by F.M. Rogallo, N.A.C.A. [No. 713], p. 165 , Lateral control required for satisfactory flying qualities based on flight tests of numerous airplanes, by R.R. Gilruth and W.N. Turner, N.A.C.A. [No. 715], p. 201 , Preignition characteristics of several fuels under simulated engine conditions, by R.C. Spencer, N.A.C.A. [No. 710], p. 121 , Pressure available for cooling with cowling flaps and tab data, by George W. Stickle, Irven Naiman, and John L. Crigler, N.A.C.A. [No. 720], p. 283 , Pressure distribution over an NACA 23021 airfoil with a slotted and a split flap, by Thomas A. Harris and John G. Lowry, N.A.C.A. [No. 718], p. 241 , Propeller analysis from experimental data, by George M. Stickle and John L. Crigler, N.A.C.A. [No. 712], p. 147 , Tests of the NACA 0025 and 0035 airfoils in the full-scale wind tunnel, by W. Kenneth Bullivant, N.A.C.A. [No. 708], p. 91 , The additional-mass effect of plates as determined by experiments, by William Gracey, N.A.C.A. [No. 707], p. 81 , The design of fins for air-cooled cylinders, by Arnold E. Biermann and Herman H. Ellerbrock, Jr. [No. 726], p. 401 , The problem of cooling an air-cooled cylinder on an aircraft engine, by M.J. Brevoort and U.T. Joyner, N.A.C.A. [No. 719], p. 267 , Wind-tunnel investigation of NACA 23012, 23021, and 23030 airfoils equipped with 40-percent-chord double-slotted flaps, by Thomas A. Harris and Isidore G. Recant, N.A.C.A. [No. 723], p. 321 , Wind-tunnel investigation of effect of interference on lateral-stability characteristics of four NACA 23012 wings, an elliptical and a circular fuselage, and vertical fins, by Rufus O. House and Arthur R. Wallace, N.A.C.A. [No. 705], p. 31 , Wind-tunnel investigation of spoiler deflector, and slot lateral-control devices on wings with full-span split and slotted flaps, by Carl J. Wenzinger and Francis M. Rogallo, N.A.C.A. [No. 706], p. 51 , © 2008 by NewsBank, Inc. All rights reserved

Language: English

URL: Volltext  (Deutschlandweit zugänglich)

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Format: 1 Online-Ressource (2 volumes)

Series Statement: Senate document No. 14

Note: vol. 1. A bill to incorporate the North Carolina Rail Road Company -- vol. 2. Amendment proposed by Mr. Joyner.

Language: English

URL: lizenzpflichtig

UID:

Format: Online-Ressource (757 p) , illustrations, tables

Edition: Online-Ausg. Chester, Vt NewsBank, inc 2008 U.S. Congressional Serial Set, 1817-1980

Series Statement: United States congressional serial set serial set no. 10471

Note: A study of air flow in an engine cylinder, by Dana W. Lee [No. 653], p. 227 , A theoretical study of the moment on a body in a compressible fluid, by Karl Caplan [No. 671], p. 581 , Air flow in the boundary layer of an elliptic cylinder, by G.B. Schubauer [No. 652], p. 207 , Aircraft rate-of-climb indicators, by Daniel P. Johnson [No. 666], p. 473 , Airfoil section data obtained in the N.A.C.A. variable-density tunnel as affected by support interference and other corrections, by Eastman N. Jacobs and Ira H. Abbott [No. 669], p. 507 , Appendix, p. 69 , Calculation of the aerodynamic characteristics of tapered wings with partial-span flaps, by Henry A. Pearson and Raymond F. Anderson [No. 665], p. 455 , Cooling on the front of an air-cooled engine cylinder in a conventional engine cowling, by M.J. Brevoort and U.T. Joyner [No. 674], p. 625 , Correction of temperatures of air-cooled engine cylinders for variation in engine and cooling conditions, by Oscar W. Schey, Benjamin Pinkel, and Herman H. Ellerbrock, Jr. [No. 645], p. 49 , Design charts for predicting downwash angles and wake characteristics behind plain and flapped wings, by Abe Silverstein and S. Katzoff [No. 648], p. 107 , Design of N.A.C.A. cowlings for radial air-cooled engines, by George W. Stickle [No. 662], p. 383 , Determination of the profile drag of an airplane wing in flight at high Reynolds numbers, by Joseph Bicknell [No. 667], p. 483 , Downwash and wake behind plain and flapped airfoils, by Abe Silverstein, S. Katzoff, and W. Kenneth Bullivant [No. 651], p. 179 , Effect of service stresses on impact resistance, x-ray diffraction patterns and microstructure of 258 aluminum alloy, by J.A. Keyes and G.W. Quick [No. 659], p. 343 , Effects of elevator nose shape, gap, balance, and tabs, on the aerodynamic characteristics of a horizontal tail surface, by Harry J. Goett and J.P. Reeder [No. 675], p. 639 , Experimental investigation of the momentum method for determining profile drag, by Harry J. Goett [No. 660], p. 643 , Experimental verification of the theory of oscillating airfoils, by Abe Silverstein and Upshur T. Joyner [No. 673], p. 619 , Freen-spinning wind-tunnel tests in a low-wing monoplane with systematic changes in wings and tails -- IV. Effect of center-of-gravity location, by Oscar Seidman and A.I. Niehouse [No. 672], p. 599 , General airplane performance, by W.C. Rockefeller [No. 654], p. 241 , Interference with tail surface and wing and fuselage from tests of 17 combinations in the N.A.C.A. variable-density tunnel, by Albert Sherman [No. 678], p. 689 , List of technical reports, p. III , Surface heat-transfer coefficients of finned cylinders, by Herman H. Ellerbrock, Jr. and Arnold E. Biermann [No. 676], p. 651 , Tensile elastic properties of 18:8 chromium-nickel steel as affected by plastic deformation, by D.J. McAdam, Jr. and R.W. Mebs [No. 670], p. 539 , Tests in the variable-density wind tunnel of the N.A.C.A. 23012 airfoil with plain and split flaps, by Ira H. Abbott and Harry Greenberg [No. 661], p. 373 , Tests of N.A.C.A. 0009, 0012, and 0018 airfoils in the full-scale tunnel, by Harry J. Goett and W. Kenneth Bullivant [No. 647], p. 97 , Tests of two full-scale propellers with different pitch distributions, at blade angles up to 60 degrees, by David Biermann and Edwin P. Hartman [No. 658], p. 327 , The "pack" method for compressive tests of thin specimens of materials used in thin-wall structures, by C.S. Aitchison and L.B. Tuckerman [No. 649], p. 133 , The aerodynamic characteristics of six full-scale propellers having different airfoil sections, by David Biermann and Edwin P. Hartman [No. 650], p. 145 , The column strength of two extruded aluminum-alloy h-sections, by William R. Osgood and Marshall Holt [No. 656], p. 289 , The compressibility burble and the effect of compressibility on pressures and forces acting on an airfoil, by John Stack, W.F. Lindsey, and Robert E. Littell [No. 646], p. 73 , The effect of Nacelle-propeller diameter ratio on body interference and on propeller and cooling characteristics, by James G. McHugh and Eldridge H. Derring [No. 680], p. 727 , The effect of continuous weathering of light metal alloys used in aircraft, by Willard Mutchler [No. 663], p. 395 , The influence of directed air flow on combustion in a spark-ignition engine, by A.M. Rothrock and R.C. Spencer [No. 657], p. 313 , The knocking characteristics of fuels in relation to maximum permissible performance of aircraft engines, by A.M. Rothrock and Arnold E. Biermann [No. 655], p. 267 , Wind-tunnel investigation of N.A.C.A. 23012, 23021, 23030 airfoils with various sizes of split flap, by Carl J. Wenzinger and Thomas A. Harris [No. 668], p. 493 , Wind-tunnel investigation of an N.A.C.A. 23012 airfoil with a slotted flap and three types of auxiliary flap, by Carl J. Wenzinger and William E. Gauvain [No. 679], p. 699 , Wind-tunnel investigation of an N.A.C.A. 23021 airfoil with various arrangements of slotted flaps, by Carl J. Wenzinger and Thomas A. Harry [No. 677], p. 665 , Wind-tunnel investigation of an N.A.C.A. 23102 airfoil with various arrangements of slotted flaps, by Carl J. Wenzinger, and Thomas A. Harris [No. 664], p. 423 , © 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)

UID:

Format: 1 Online-Ressource (2 volumes)

Series Statement: Senate doc 80-81

Note: "Senate, Dec. 21, 1850. Introduced by Mr. Joyner."--Vol. 2, title page verso , vol. 1. Report -- vol. 2. A bill to incorporate the Raleigh and Gaston Railroad Company.

Additional Edition: Erscheint auch als Druck-Ausgabe North Carolina. General Assembly. Senate. Select Committee on the Resolution Relating to the Raleigh and Gaston Railroad Report of the Select Committee on the resolution relating to the Raleigh and Gaston Railroad Raleigh : Thomas J. Lemay, printer to the State

Language: English

URL: lizenzpflichtig