Kooperativer Bibliotheksverbund

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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

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)

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Format: 1 online resource (14 pages, 9 unnumbered pages) : , illustrations.

Series Statement: Technical note / National Advisory Committee for Aeronautics ; No. 426

Note: "July, 1932 , No Federal Depository Library Program (FDLP) item number.

Language: English

UID:

Format: 1 online resource (14 pages, 9 unnumbered pages) : , illustrations.

Series Statement: Technical note / National Advisory Committee for Aeronautics ; No. 426

Note: "July, 1932 , No Federal Depository Library Program (FDLP) item number.

Language: English

UID:

Format: 1 online resource (12 pages, 12 unnumbered pages) : , illustrations.

Series Statement: Technical note / National Advisory Committee for Aeronautics ; No. 558

Note: "March 1936." , No Federal Depository Library Program (FDLP) item number.

Language: English

UID:

Format: 1 online resource (18 pages, 13 unnumbered pages) : , illustrations.

Series Statement: Technical note / National Advisory Committee for Aeronautics ; no. 816

Note: "July 1941." , No Federal Depository Library Program (FDLP) item number.

Language: English

UID:

Format: 1 online resource (18 pages, 13 unnumbered pages) : , illustrations.

Series Statement: Technical note / National Advisory Committee for Aeronautics ; no. 816

Note: "July 1941." , No Federal Depository Library Program (FDLP) item number.

Language: English

UID:

Format: 1 online resource (19 pages, 11 unnumbered pages) : , illustrations.

Series Statement: Technical note / National Advisory Committee for Aeronautics ; No. 572

Note: "July 1936." , No Federal Depository Library Program (FDLP) item number.

Language: English

UID:

Format: 1 online resource (12 pages, 12 unnumbered pages) : , illustrations.

Series Statement: Technical note / National Advisory Committee for Aeronautics ; No. 558

Note: "March 1936." , No Federal Depository Library Program (FDLP) item number.

Language: English

UID:

Format: 1 online resource (19 pages, 11 unnumbered pages) : , illustrations.

Series Statement: Technical note / National Advisory Committee for Aeronautics ; No. 572

Note: "July 1936." , No Federal Depository Library Program (FDLP) item number.

Language: English