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Format: Online-Ressource (657 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. 9911

Note: A description and test results of a spark-ignition and a compression-ignition 2-stroke cycle engine, by J.A. Spanogle and E.G. Whitney [No. 495], p. 395 , A flight investigation of the effect of mass distribution and control setting on the spinning of the XN2Y-1 airplane, by N.F. Scudder [No. 484], p. 185 , A flight investigation of the lateral control characteristics of short wide ailerons and various spoilers with different amounts of wing dihedral, by Fred E. Weick, Hartley A. Soule, and Melvin N. Gough [No. 494], p. 381 , Air conditions close to the ground and the effect on airplane landings, by F.L. Thompson, W.C. Peck, and A.P. Beard [No. 489], p. 271 , An aerodynamic analysis of the autogiro rotor with a comparison between calculated and experimental results, by John B. Wheatley [No. 487], p. 235 , Computation of the two-dimensional flow in a laminar boundary layer, by Hugh L. Dryden [No. 497], p. 435 , Effect of moderate air flow on the distribution of fuel sprays after injection cut-off, by A.M. Rothrock and R.C. Spencer [No. 483], p. 163 , Effect of viscosity on fuel leakage between lapped plungers and sleeves and on the discharge from a pump-injection system, by A.M. Rothrock and E.T. Marsh [No. 477], p. 63 , Experimental verification of the theory of wind-tunnel boundary interference, by Theodore Theodorsen and Abe Silverstein [No. 478], p. 79 , General theory of aerodynamic instability and the mechanism of flutter, by Theodore Theodorsen [No. 496], p. 413 , Heat transfer from finned metal cylinders in an air stream, by Arnold E. Biermann and Benjamin Pinkel [No. 488], p. 251 , Improved airplane windshields to provide vision in stormy weather, by William C. Clay [No. 498], p. 445 , Infrared radiation from explosions in a spark-ignition engine, by Charles F. Marvin, Jr., Frank R. Caldwell, and Sydney Steele [No. 486], p. 223 , List of technical reports, p. VII , On the theory of laminar boundary layers involving separation, by Th. von Karman and C.B. Milliken [No. 504], p. 541 , Relation of hydrogen and methane to carbon monoxide in exhaust gases from internal combustion engines, by Harold C. Gerrish and Arthur M. Tessmann [No. 476], p. 53 , Relative loading on biplane wings of unequal chords, by Walter S. Diehl [No. 501], p. 503 , Scale effect on Clark V airfoil characteristics from N.A.C.A. full-scale wind-tunnel tests, by Abe Silverstein [No. 502], p. 509 , Stability of thin-walled tubes under torsion, by L.H. Donnell [No. 479], p. 95 , Tests of nacelle-propeller combinations in various positions in reference to wings. IV. -- Thick wing -- various radial engine cowlings -- tandem propellers, by James G. McHugh [No. 505], p. 561 , Tests of 16 related airfoils at high speeds, by John Stack and Albert B. von Doenhoff [No. 492], p. 339 , Tests of nacelle-propeller combinations in various positions in reference to wings. V. -- Clark Y biplane cellule -- N.A.C.A. cowled nacelle -- tractor propeller, by E. Floyd Valentine [No. 506], p. 603 , Tests of nacelle-propeller combinations in various positions with reference to wings. VI. -- Wings and nacelles with pusher propeller, by Donald H. Wood and Carlton Bioletti [No. 507], p. 619 , The aerodynamic effects of wing cut-outs, by Albert Sherman [No. 480], p. 117 , The drag of airplane wheels, wheel fairings, and landing gears-I, by William H. Herrnstein, Jr. and David Biermann [No. 485], p. 193 , The effect of spray strips on the take-off performance of a model of a flying boat hull, by Starr Truscott [No. 503], p. 523 , The influence of tip shape on the wing-load distribution as determined by flight tests, by Richard V. Rhode [No. 500], p. 479 , The physical effects of detonation in a closed cylindrical chamber, by C.S. Draper [No. 493], p. 361 , The weathering of aluminum alloy sheet materials used in aircraft, by Willard Mutchler [No. 490], p. 285 , Vibration response of airplane structures, by T. Theodorsen and A.G. Gelalles [No. 491], p. 319 , Wind tunnel research comparing lateral control devices, particularly at high angles of attack. XII. -- Upper surface ailerons on wings with split flaps, by Fred E. Weick and Carl J. Wenzinger [No. 499], p. 463 , Wing pressure distribution and rotor-blade motion of an autogiro as determined in flight, by John B. Wheatley [No. 475], p. 43 , Wing-fuselage interference, tail buffeting, and air flow about the tail of a low-wing monoplane, by James A. White and Manley J. Hood [No. 482], p. 143 , Working charts for the determination of propeller thrust at various air speeds, by Edwin P. Hartman [No. 481], p. 123 , © 2007 by NewsBank, Inc. All rights reserved

Language: English

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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

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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

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Format: Online-Ressource (532 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. 10576

Note: A theoretical study of lateral stability with an automatic pilot, by Frederick H. Imlay, N.A.C.A. [No. 693], p. 273 , Aerodynamic characteristics of horizontal tail surfaces, by Abe Silverstein and S. Katzoff, N.A.C.A. [No. 688], p. 175 , Appendix, p. 80 , Correlation of cooling data from an air-cooled cylinder and several multicylinder engines, by Benjamin Pinkel and Herman H. Ellenbrock, Jr., N.A.C.A. [No. 683], p. 59 , Design charts relating to the stalling of tapered wings, by H.A. Soule and R.F. Anderson, N.A.C.A. [No. 703], p. 513 , Determination of ground effect from tests of a gilder in towed flight, by J.W. Wetmore and L.I. Turner, Jr., N.A.C.A. [No. 695], p. 295 , Effect of exit-slot position and opening on the available cooling pressure for N.A.C.A. nose-slot cowlings, by George W. Stickle, Irven Naiman, and John L. Crigler, N.A.C.A. [No. 687], p. 163 , Effect of fuel-air ratio, inlet temperature and exhaust pressure on detonation, by E.S. Taylor, W.A. Leary, and J.R. Diver, Massachusetts Institute of Technology [No. 699], p. 423 , Effective gust structure of low altitudes as determined from the reactions of an airplane, by Philip Donely, N.A.C.A. [No. 692], p. 263 , Flame speeds and energy considerations for explosions in a spherical bomb, by Ernest F. Fiock, Charles F. Marvin, Jr., Frank R. Caldwell, and Carl H. Roeder, N.A.C.A. [No. 682], p. 39 , Free-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails. V. Effect of airplane relative density, by Oscar Seidman and A.I. Neihouse, N.A.C.A. [No. 691], p. 243 , Investigations on the incompletely developed plane diagonal-tension field, by Paul Kuhn, N.A.C.A. [No. 697], p. 387 , Longitudinal stability and control with special reference to slipstream effects, by S. Katzoff, N.A.C.A. [No. 690], p. 213 , Mechanical properties of flush-riveted joints, by W.C. Brueggeman and Frederick C. Roop, National Bureau of Standards [No. 701], p. 467 , Mechanism of flutter: A theoretical and experimental investigation of the flutter problem, by Theodore Theodorsen and I.E. Garrick, N.A.C.A. [No. 685], p. 101 , Piston temperatures in an air-cooled engine for various operating conditions, by Eugene J. Manganiello, N.A.C.A. [No. 698], p. 413 , Preliminary investigation of the flying qualities of airplanes, by H.A. Soule, N.A.C.A. [No. 700], p. 449 , Preliminary wind-tunnel investigation of an N.A.C.A. 23012 airfoil with various arrangements of Venetian-blind flaps, by Carl J. Wenzinger and Thomas A. Harris, N.A.C.A. [No. 689], p. 197 , Stability of castering wheels for aircraft landing gears, by Arthur Kantrowitz, N.A.C.A. [No. 686[, p. 147 , Static thrust and power characteristics of six full-scale propellers, by Edwin P. Hartman and David Biermann, N.A.C.A. [No. 684], p. 85 , Tensile elastic properties of typical stainless steels and nonferrous metals as affected by plastic deformation and by heat treatment, by D.J. McAdam, Jr., and R.W. Mebs, National Bureau of Standards [No. 696], p. 309 , The application of basic data on planing surfaces to the design of flying-boat hulls, by Walter S. Diehl, Bureau of Aeronautics, Navy Department [No. 694], p. 287 , The calculated effect of various hydrodynamic and aerodynamic factors on the take off of a large flying boat, by R.E. Olson and J.M. Allison, N.A.C.A. [No. 702], p. 497 , The unsteady lift of a wing of finite aspect ratio, by Robert T. Jones, N.AC.A. [No. 681), p. 31 , © 2008 by NewsBank, Inc. All rights reserved

Language: English

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Format: Online-Ressource (432 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. 10825

Note: A study by high-speed photography of combustion and knock in a spark-ignition engine, by Cearcy D. Miller [No. 727], p. 15 , An investigation of the drag of windshields in 8-foot high-speed wind-tunnel, by Russell G. Robinson and James B. Delano [No. 730], p. 65 , Bending of rectangular plates with large deflections, by Samuel Levy [No. 737], p. 139 , Critical compressive stress for flat rectangular plates supported along all edges and elastically restrained against rotation along the unloaded edges, by Eugene E. Lundquist and Elbridge Z. Stowell [No. 733], p. 99 , Critical compressive stress for outstanding flanges, by Eugene E. Lundquist and Elbridge Z. Stowell [No. 734], p. 111 , Determination of optimum plan forms for control surfaces, by Robert T. Jones and Doris Cohen [No. 731], p. 79 , Drag and propulsive characteristics of air-cooled engine-nacelle installations for large airplanes, by Abe Silverstein and Herbert A. Wilson, Jr. [No. 746], p. 301 , Flutter calculations in three degrees of freedom, by Theodore Theodorsen and I.E. Garrick [No. 741], p. 223 , Ground effect on downwash angles and wake location, by S. Katzoff and Harold H. Sweberg [No. 738], p. 159 , High-speed tests of a model twin-engine low-wing transport airplane, by John V. Becker and Lloyd H. Leonard [No. 750], p. 391 , High-speed tests of conventional radial-engine cowlings, by Russell G. Robinson and John V. Becker [No. 745], p. 287 , Investigation in the 7-by 10-foot wind-tunnel of ducts for cooling radiators within an airplane wing, by Thomas A. Harris and Isidore G. Recant [No. 743], p. 249 , List of technical reports, p. III , Non-stationary flow about a wing-aileron tab combination including aerodynamic balance, by Theodore Theodorsen and I.E. Garrick [No. 736], p. 129 , Normal pressure tests of circular plates with clamped edges, by Albert E. McPherson, Walter Ramberg, and Samuel Levy [No. 744], p. 269 , Normal-pressure tests of rectangular plates, by Walter Ramberg, Albert E. McPherson, and Samuel Levy [No. 748], p. 349 , On the use of residue theory for treating the subsonic flow of a compressible fluid, by Carl Kaplan [No. 728], p. 39 , Pressure distribution over an NACA 23012 airfoil with a fixed slot and a slotted flap, by Thomas A. Harris and John G. Lowry [No. 732], p. 85 , Propeller charts for the determination of the rotational speed for the maximum ration of the propulsive efficiency to the specific fuel consumption, by David Biermann and Robert N. Conway [No. 749], p. 373 , Restraint provided a flat rectangular plate by a study stiffener along an edge of the plate, by Eugene E. Lundquist and Elbridge Z. Stowell [No. 735], p. 123 , Shear lag in box beams: Methods of analysis and experimental investigations, by Paul Kuhn and Patrick T. Chiarito [No. 739], p. 171 , Square plate with clamped edges under normal pressure producing large deflections, by Samuel Levy [No. 740], p. 209 , Test of a single-stage axial flow-fan, by E. Barton Bell [No. 729], p. 49 , The mean aerodynamic chord and the aerodynamic center of a tapered wing, by Walter S. Diehl [No. 751], p. 413 , Wind-tunnel investigation of an NACA 23012 airfoil with 30-percent-chord venetian-blind flaps, by F.M. Rogallo and Bartholomew S. Spano [No. 742], p. 241 , Wind-tunnel tests of four- and six-blade single- and dual-rotating tractor propellers, by David Biermann and Edwin P. Hartman [No. 747], p. 319 , © 2008 by NewsBank, Inc. All rights reserved

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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

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