%0 Generic

%T Twenty-fifth annual report of the National Advisory Committee for Aeronautics, 1939, including technical reports Nos. 645 to 680

%A United States Congress Senate

%A United States National Advisory Committee for Aeronautics

%A Abbott, Ira H.A

%A Aitchison, C.S

%A Anderson, Raymond F.

%A Bicknell, Joseph

%A Biermann, Arnold E.

%A Biermann, David

%A Brevoort, Maurice J.

%A Bullivant, W. Kenneth

%A Caplan, Karl

%A Derring, Eldridge H.

%A Ellerbrock, Herman H.

%A Gauvain, William E.

%A Goett, Harry J.

%A Greenberg, Harry

%A Harris, Thomas A.

%A Hartman, Edwin P.

%A Holt, Marshall

%A Jacobs, Eastman N.

%A Johnson, Daniel Palmer

%A Niehouse, A.I

%A Rothrock, A.M

%A Silverstein, Abe

%A Sherman, Albert

%A Pinkel, Benjamin

%A Wenzinger, Carl J.

%A Lee, Dana W.

%A Quick, G.W

%A Schubauer, Galen Brandt

%A Stickle, George W.

%A Pearson, Henry A.

%A Kies, J.A

%A Reeder, J.P

%A McHugh, James G.

%A Stack, John

%A Tuckerman, L.B

%A Seidman, Oscar

%A Schey, Oscar W.

%A Mebs, R.W

%A Spencer, Robert C.

%A Littell, Robert E.

%A Katzoff, S.

%A Joyner, Upshur T.

%A Rockefeller, W.C

%A Lindsey, W.F

%A Mutchler, Willard

%A Osgood, William R.

%A McAdam, D.J

%D 1940

%X A study of air flow in an engine cylinder, by Dana W. Lee [No. 653], p. 227

%X A theoretical study of the moment on a body in a compressible fluid, by Karl Caplan [No. 671], p. 581

%X Air flow in the boundary layer of an elliptic cylinder, by G.B. Schubauer [No. 652], p. 207

%X Aircraft rate-of-climb indicators, by Daniel P. Johnson [No. 666], p. 473

%X 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

%X Appendix, p. 69

%X Calculation of the aerodynamic characteristics of tapered wings with partial-span flaps, by Henry A. Pearson and Raymond F. Anderson [No. 665], p. 455

%X 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

%X 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

%X Design charts for predicting downwash angles and wake characteristics behind plain and flapped wings, by Abe Silverstein and S. Katzoff [No. 648], p. 107

%X Design of N.A.C.A. cowlings for radial air-cooled engines, by George W. Stickle [No. 662], p. 383

%X Determination of the profile drag of an airplane wing in flight at high Reynolds numbers, by Joseph Bicknell [No. 667], p. 483

%X Downwash and wake behind plain and flapped airfoils, by Abe Silverstein, S. Katzoff, and W. Kenneth Bullivant [No. 651], p. 179

%X 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

%X 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

%X Experimental investigation of the momentum method for determining profile drag, by Harry J. Goett [No. 660], p. 643

%X Experimental verification of the theory of oscillating airfoils, by Abe Silverstein and Upshur T. Joyner [No. 673], p. 619

%X 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

%X General airplane performance, by W.C. Rockefeller [No. 654], p. 241

%X 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

%X List of technical reports, p. III

%X Surface heat-transfer coefficients of finned cylinders, by Herman H. Ellerbrock, Jr. and Arnold E. Biermann [No. 676], p. 651

%X 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

%X 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

%X 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

%X 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

%X 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

%X The aerodynamic characteristics of six full-scale propellers having different airfoil sections, by David Biermann and Edwin P. Hartman [No. 650], p. 145

%X The column strength of two extruded aluminum-alloy h-sections, by William R. Osgood and Marshall Holt [No. 656], p. 289

%X 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

%X 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

%X The effect of continuous weathering of light metal alloys used in aircraft, by Willard Mutchler [No. 663], p. 395

%X 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

%X 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

%X 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

%X 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

%X 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

%X 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

%C Washington, DC

%U http://slubdd.de/katalog?TN_libero_mab2