Kooperativer Bibliotheksverbund

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Format: Online-Ressource (582 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. 9003

Note: A preliminary investigation of supercharging an air-cooled engine in flight, by Marsden Ware and Oscar W. Schey [No. 283], p. 81 , A study of wing flutter, by A.F. Zahm and R.M. Bear [No. 285], p. 107 , Aerodynamic characteristics of airfoils-V, by National Advisory Committee for Aeronautics [No. 286], p. 135 , Aircraft accidents, by Special Subcommittee of the National Advisory Committee for Aeronautics [No. 308], p. 557 , An investigation of the aerodynamic characteristics of an airplane equipped with several different sets of wings, by J.W. Crowley, Jr., and M.W. Green [No. 303], p. 477 , An investigation of the aerodynamic characteristics of an airplane equipped with several different sets of wings, by J.W. Crowley, Jr., and M.W. Green [No. 304], p. 487 , An investigation of the use of discharge valves and intake control for improving the performance of N.A.C.A. Roots Type Supercharger, by Oscar W. Schey and Ernest E. Wilson [No. 302], p. 477 , Characteristics of five propellers in flight, by J.W. Crowley, Jr., and R.E. Mixson [No. 292], p. 265 , Drag of C-class airship hulls of various fineness ratios, by A.F. Zahm, R.H. Smith, and F.A. Louden [No. 291], p. 249 , Effect of variation of chord and span of ailerons on rolling and yawing moments in level flight, by R.H. Heald and D.H. Strother [No. 298], p. 383 , Forces on elliptic cylinders in uniform air stream, by A.F. Zahm, R.H. Smith, and F.A. Louden [No. 289], p. 215 , Full scale tests on a thin metal propeller at various tip speeds, by Fred E. Weick [No. 301], p. 463 , Full-scale wind-tunnel tests of a series of metal propellers on a VE-7 airplane, by Fred E. Weick [No. 306], p. 519 , Investigation of damping liquids for aircraft instruments, by G.H. Keulegan [No. 299], p. 403 , Pressure distribution over a rectangular monoplane wing model up to 90' angle of attack, by Montgomery Knight and Ocsar Loeser, Jr. [No. 288], p. 195 , Pressure distribution tests on PW-9 models from -18' through 90' angle of attack, by Oscar E. Loeser, Jr. [No. 296], p. 333 , Reduction of observed airplane performance to standard conditions, by Walter S. Diehl [No. 297], p. 355 , Table of contents, p. VI , The comparative performance of roots type aircraft engine superchargers as affected by change in impeller speed and displacement, by Marsden Ware and Ernest E. Wilson [No. 284], p. 93 , The gaseous explosive reaction: A study of the kinetics of composite fuels, by F.W. Stevens [No. 305], p. 501 , The measurement of maximum cylinder pressures, by Chester W. Hicks [No. 294], p. 309 , The pressure distribution over the horizontal and vertical tail surfaces of the F6C-4 pursuit airplane in violent maneuvers, by R.V. Rhode [No. 307], p. 537 , The twenty-foot propeller research tunnel of the National Advisory Committee for Aeronautics, by Fred E. Weick and Donald H. Wood [No. 300], p. 427 , The variation in engine power with altitude determined from measurements in flight with a hub dynamometer, by W.D. Gove [No. 295], p. 321 , Theories of flow similitude, by A.F. Zahm [No. 287], p. 185 , Two practical methods for the calculation of the horizontal tail area necessary for a statically stable airplane, by Walter S. Diehl [No. 293], p. 289 , Water-pressure distribution on a seaplane float, by F.L. Thompson [No. 290], p. 233 , © 2007 by NewsBank, Inc. All rights reserved

Language: English

URL: Volltext  (Deutschlandweit zugänglich)

UID:

Format: Online-Ressource (799 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. 9348

Note: A method of calculating the ultimate strength of continuous beams, by J.A. Newlin and George W. Trayer [No. 347], p. 291 , A proof of the theorem regarding the distribution of lift over the span for minimum induced drag, by W.F. Durand [No. 349], p. 361 , Aircraft accidents: Method of analysis, by Committee on Aircraft Accidents of the National Advisory Committee for Aeronautics [No. 357], p. 539 , Aircraft woods: Their properties, selection, and characteristics, by L.J. Markwardt [No. 354], p. 467 , Airfoil pressure distribution investigation in the variable density wind tunnel, by Eastman N. Jacobs, John Stack, and Robert M. Pinkerton [No. 353], p. 451 , An extended theory of thin airfoils and its application to the biplane problem, by Clark B. Millikan [No. 362], p. 635 , An investigation of the effectiveness of ignition sparks, by Melville F. Peters, Wayne L. Summerville, and Merlin Davis [No. 359], p. 573 , Comparative flight performance with an N.A.C.A. roots supercharger and a turbocentrifugal supercharger, by Oscar W. Schey and Alfred W. Young [No. 355], p. 501 , Effect of turbulence in wind tunnel measurements, by H.L. Dryden and A.M. Kuethe [No. 342], p. 145 , Effect of variation of chord and span of ailerons on rolling and yawing moments at several angles of pitch, by R.H. Heald, D.H. Strother, and B.H. Monish [No. 343], p. 171 , Experimental determination of jet boundary corrections for airfoil tests in four open wind tunnel jets of different shapes, by Montgomery Knight and Thomas A. Harris [No. 361], p. 607 , Full scale wind tunnel tests of a propeller with the diameter changed by cutting off the blade tips, by Donald H. Wood [No. 351], p. 393 , Full scale wind tunnel tests on several metal propellers having different blade forms, by Fred E. Weick [No. 340], p. 121 , Full scale wind tunnel tests with a series of propellers of different diameters on a single fuselage, by Fred E. Weick [No. 339], p. 105 , Large scale aerodynamic characteristics of airfoils as tested in the variable density wind tunnel, by Eastman N. Jacobs and Raymond F. Anderson [No. 352], p. 419 , List of technical reports, p. VII , Pressure distribution over a symmetrical airfoil section with trailing edge flap, by Eastman N. Jacobs and Robert M. Pinkerton [No. 360], p. 587 , Pressure fluctuations in a common-rail fuel injection system, by A.M. Rothrock [No. 363], p. 669 , Strength of rectangular flat plates under edge compression, by Louis Schuman and Goldie Black [No. 356], p. 515 , Strength of welded joints in tubular members for aircraft, by H.L. Whittemore and W.C. Brueggeman [No. 348], p. 319 , Table of contents, p. VI , Temperature coefficient of the modulus of rigidity of aircraft instrument diaphragm and spring materials, by W.G. Brombacher and E.R. Melton [No. 358], p. 557 , The design and development of an automatic injection valve with an annular orifice of varying area, by William F. Joachim, Chester W. Hicks, and Hampton H. Foster [No. 341], p. 135 , The design of airplane wing ribs, by J.A. Newlin and George W. Trayer [No. 345], p. 219 , The design of plywood webs for airplane wing beams, by George W. Trayer [No. 344], p. 201 , The effect of reduction gearing on propeller-body interference as shown by full scale wind tunnel tests, by Fred E. Weick [No. 338], p. 83 , The gaseous explosive reaction at constant pressure -- the reaction order and reaction rate, by F.W. Stevens [No. 337], p. 67 , The pressure distribution over the wings and tail surfaces of a PW-9 pursuit airplane in flight, by Richard V. Rhode [No. 364], p. 685 , Water pressure distribution on a flying boat hull, by F.L. Thompson [No. 346], p. 273 , Working charts for the selection of aluminum alloy propellers of a standard form to operate with various aircraft engines and bodies, by Fred E. Weick [No. 350], p. 377 , © 2007 by NewsBank, Inc. All rights reserved

Language: English

URL: Volltext  (Deutschlandweit zugänglich)

UID:

Format: Online-Ressource (645 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. 9802

Note: A comparison between the theoretical and measured longitudinal stability characteristics of an airplane, by Hartley A. Soule and John B. Wheatley [No. 442], p. 53 , A flight investigation of the spinning of the NY-1 airplane with varied mass distribution and other modifications, and an analysis based on wind-tunnel tests, by Nathan F. Schudder [No. 441], p. 37 , Aircraft power-plant instruments, by Harcourt Sontag and W.G. Brombacher [No. 466], p. 447 , Airfoil section characteristics as affected by protuberances, by Eastman N. Jacobs [No. 446], p. 109 , Appendix, p. 65 , Determination of the theoretical pressure distribution for twenty airfoils, by I.E. Garrick [No. 465], p. 433 , General potential theory of arbitrary wing sections, by T. Theodorsen and I.E. Garrick [No. 452], p. 177 , Improved apparatus for the measurement of fluctuations of air speed in turbulent flow, by W.C. Mock, Jr. and H.L. Dryden [No. 448], p. 131 , Increasing the air charge and scavenging the clearance volume of a compression-ignition engine, by J.S. Spanogle, C.W. Hicks, and H.H. Foster [No. 469], p. 525 , Interference on an airfoil of finite span in an open rectangular wind tunnel, by Theodore Theodoresen [No. 561], p. 355 , List of technical reports, p. VII , Maneuverability investigation of O3U-1 observation airplane, by F.L. Thompson and H.W. Kirschbaum [No. 457], p. 263 , Negative thrust and torque characteristics of an adjustable-pitch metal propeller, by Edwin P. Hartmen [No 464], p. 421 , Nomenclature for aeronautics, by National Advisory Committee for Aeronautics [No. 474], p. 603 , Penetration and duration of fuel sprays from a pump injection system, by A.M. Rothrock and E.T. March [No. 455], p. 241 , Performance of a fuel-injection spark-ignition engine using a hydrogenated safety fuel, by Oscar W. Schey and Alfred W. Young [No. 471], p. 557 , Photomicrographic studies of fuel sprays, by Dana W. Lee and Robert C. Spencer [No. 454], p. 215 , Pressure-distribution measurements on the hull and fins of a 1/40-scale model of the U.S. airship Akron, by Hugh B. Freeman [No. 443], p. 67 , Relative loading on biplane wings, by Walter S. Diehl [No. 458], p. 275 , Static thrust of airplane propellers, by Walter S. Diehl [No. 447], p. 125 , Strength tests of thin-walled duralumin cylinders in compression, by Eugene E. Lundquist [No. 473], p. 585 , Tests of nacelle-propeller combinations in various positions with reference to wings. III. -- Clark Y wing -- Various radial-engine cowlings -- Tractor propeller, by Donald H. Wood [No. 462], p. 359 , The N.A.C.A. full-scale wind tunnel, by Smith J. De France [No. 459], p. 291 , The N.A.C.A. high-speed wind tunnel and tests of six propeller sections, by John Stack [No. 463], p. 399 , The N.A.C.A. tank: A high-speed towing basin for testing models of seaplane floats, by Starr Truscott [No. 470], p. 535 , The aerodynamic forces and moments exerted on a spinning model of the NY-1 airplane as measured by the spinning balance, by M.J. Bamber and C.H. Zimmerman [No. 456], p. 249 , The calculation of take-off run, by Walter S. Diehl [No. 450], p. 163 , The characteristics of 78 related airfoil sections from tests in the variable-density wind tunnel, by Eastman N. Jacobs, Kenneth E. Ward, and Robert M. Pinkerton [No. 460], p. 299 , The drag of two streamline bodies as affected by protuberances and appendages, by Ira H. Abbot [No. 451], p. 171 , The estimation of maximum load capacity of seaplanes and flying boats, by Walter S. Diehl [No. 453], p. 211 , The experimental determination of the moments of inertia of airplanes, by Hartley A. Soule and Marvel P. Miller [No. 467], p. 501 , The interference between struts in various combinations, by David Biermann and William H. Herrnstein, Jr. [No. 468], p. 515 , Wind-tunnel research comparing lateral control devices particularly at high angles of attack. VI. -- Skewed ailerons and rectangular wings, by Fred E. Weick and Thomas A. Harris [No. 444], p. 81 , Wind-tunnel tests on combinations of a wing with fixed auxiliary airfoils having various chords and profiles, by Fred E. Weick and Robert Sanders [No. 472], p. 567 , Wing characteristics as affected by protuberances of short span, by Eastman N. Jacobs and Albert Sherman [No. 449], p. 155 , Working charts for the determination of the lift distribution between biplane wings, by Paul Kuhn [No. 445], p. 93 , © 2007 by NewsBank, Inc. All rights reserved

Language: English

URL: Volltext  (Deutschlandweit zugänglich)

UID:

Format: 1 online resource (11 pages, 4 unnumbered pages) : , illustrations.

Series Statement: Technical notes / National Advisory Committee for Aeronautics ; No. 298

Note: "September 1928." , No Federal Depository Library Program (FDLP) item number.

Language: English

UID:

Format: 1 online resource (11 pages, 4 unnumbered pages) : , illustrations.

Series Statement: Technical notes / National Advisory Committee for Aeronautics ; No. 298

Note: "September 1928." , No Federal Depository Library Program (FDLP) item number.

Language: English