Twenty-fourth annual report of the National Advisory Committee for Aeronautics, 1938. Including technical reports nos. 612 to 644. [electronic resource]

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Corporate Authors: United States. Congress. Senate, United States. National Advisory Committee for Aeronautics
Other Authors: Allen, H. Julian, Anderson, Raymond F., Anderson, Walter B., Bailey, F.J, Becker, John Vernon, 1913-, Biermann, David, Delano, James B. (James Benjamin), Diehl, Walter S. (Walter Stuart), 1893-1976, Garrick, I. E. (Isadore Edward), 1910-1981, Gerrish, Harold C., Gracey, William, 1913-, Greenberg, Harry, Hartman, Edwin Phelps, 1905-, Hootman, J. A. (James A.), Jacobs, Eastman N. (Eastman Nixon), 1902-1987, Jones, Robert T. (Robert Thomas), 1910-1999, Kaplan, Carl, Katzoff, S. (Samuel), 1909-, Kuhn, Paul, Lindsey, W. F., Osgood, William R., Pearson, Henry A. (Henry Adolph), 1906-, Pinkel, Benjamin, 1909-, Pinkerton, Robert M., Rhode, Richard V., Rothrock, A. M. (Addison May), 1903-1971, Selden, Robert F., Silverstein, Abe, Soule, Hartley A. (Hartley Akin), 1904-1988, Spencer, Robert C. (Robert Champlin), 1926-, Voss, Fred, Wenzinger, Carl J. (Carl Joseph), 1903-1988, Wetmore, J. W. (Joseph W.)
Format: Government Document Electronic eBook
Language:English
Published: Washington, DC, 1939.
Series:United States congressional serial set ; serial set no. 10318.
Senate document (United States. Congress. Senate) ; 76th Congress, no. 3.
Subjects:

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110 1 |a United States.  |b Congress.  |b Senate. 
245 1 0 |a Twenty-fourth annual report of the National Advisory Committee for Aeronautics, 1938. Including technical reports nos. 612 to 644.  |h [electronic resource] 
260 |a Washington, DC,  |c 1939. 
300 |a 643 p. :  |b illustrations, tables. 
440 0 |a United States congressional serial set ;  |v serial set no. 10318. 
490 1 |a Senate document / 76th Congress, 1st session. Senate ;  |v no. 3. 
500 |a List of technical reports, p. III. 
500 |a Heat-transfer processes in air-cooled engine cylinders, by Benjamin Pinkel [No. 612], p. 49. 
500 |a The variation with Reynolds number of pressure distribution over an airfoil section, by Robert M. Pinkerton [No. 613], p. 65. 
500 |a 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. 
500 |a Column strength of tubes elastically restrained against rotation at the ends, by William R. Osgood [No. 615], p. 101. 
500 |a Interrelation of exhaust-gas constituents, by Harold C. Gerrish and Fred Voss [No. 616], p. 139. 
500 |a Auto-ignition and combustion of diesel fuel in a constant-volume bomb, by Robert F. Selden [No. 617], p. 147. 
500 |a 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. 
500 |a Drag of cylinders of simple shapes, by W.F. Lindsey [No. 619], p. 169. 
500 |a Pressure distribution over airfoils with Fowler flaps, by Carl J. Wenzinger and Walter B. Anderson [No. 620], p. 177. 
500 |a Compressible flow about symmetrical Jonkowski profiles, by Carl Kaplan [No. 621], p. 197. 
500 |a A photographic study of combustion and knock in a spark-ignition engine, by A.M. Rothrock and R.C. Spencer [No. 622], p. 213. 
500 |a A study of the torque equilibrium of an auto-giro rotor, by F.J. Bailey, Jr. [No. 623], p. 235. 
500 |a Two dimensional subsonic compressible flow past elliptical cylinders, by Carl Kaplan [No. 624], p. 245. 
500 |a 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. 
500 |a The transition phase in the take-off of an airplane, by J.W. Wetmore [No. 626], p. 261. 
500 |a The experimental and calculated characteristics of 22 tapered wings, by Raymond F. Anderson [No. 627], p. 273. 
500 |a 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. 
500 |a On sonic reciprocal relations in the theory of nonstationary flows, by I.E. Garrick [No. 629], p. 347. 
500 |a 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. 
500 |a 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. 
500 |a The crinkling strength and the bending strength of round aircraft tubing, by William R. Osgood [No. 632], p. 387. 
500 |a 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. 
500 |a 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. 
500 |a 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. 
500 |a Approximate stress analysis of multistringer beams with shear deformation of the flanges, by Paul Kuhn [No. 636], p. 469. 
500 |a 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. 
500 |a 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. 
500 |a 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. 
500 |a 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. 
500 |a 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. 
500 |a 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. 
500 |a The aerodynamic characteristics of four full-scale propellers having different plan forms, by Edwin P. Hartman and David Biermann [No. 643], p. 617. 
500 |a 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. 
500 |a Appendix, p. 130. 
533 |a Electronic reproduction.   |b Chester, Vt.:   |c NewsBank, inc.,   |d 2007.   |n Available via the World Wide Web.   |n Access restricted to Readex U.S. Congressional Serial Set subscribers. 
540 |a Copyright 2008 by NewsBank, Inc. All rights reserved. 
610 1 7 |a United States.  |b National Advisory Committee for Aeronautics.  |2 Readex congressional thesaurus. 
650 0 7 |a Aeronautics.  |2 Readex congressional thesaurus. 
650 0 7 |a Aircraft accidents and safety.  |2 Readex congressional thesaurus. 
650 0 7 |a Aircraft construction.  |2 Readex congressional thesaurus. 
650 0 7 |a Aircraft engines.  |2 Readex congressional thesaurus. 
650 0 7 |a Aircraft industry.  |2 Readex congressional thesaurus. 
650 0 7 |a Aircraft parts.  |2 Readex congressional thesaurus. 
650 0 7 |a Airplanes.  |2 Readex congressional thesaurus. 
650 0 7 |a Strength of materials.  |2 Readex congressional thesaurus. 
650 0 7 |a Transportation research.  |2 Readex congressional thesaurus. 
650 0 7 |a Wind tunnels.  |2 Readex congressional thesaurus. 
655 7 |a Annual Reports.  |2 Readex congressional thesaurus. 
655 7 |a Monographs.  |2 Readex congressional thesaurus. 
700 1 |a Allen, H. Julian. 
700 1 |a Anderson, Raymond F. 
700 1 |a Anderson, Walter B. 
700 1 |a Bailey, F.J. 
700 1 |a Becker, John Vernon,  |d 1913- 
700 1 |a Biermann, David. 
700 1 |a Delano, James B.  |q (James Benjamin) 
700 1 |a Diehl, Walter S.  |q (Walter Stuart),  |d 1893-1976. 
700 1 |a Garrick, I. E.  |q (Isadore Edward),  |d 1910-1981. 
700 1 |a Gerrish, Harold C. 
700 1 |a Gracey, William,  |d 1913- 
700 1 |a Greenberg, Harry. 
700 1 |a Hartman, Edwin Phelps,  |d 1905- 
700 1 |a Hootman, J. A.  |q (James A.) 
700 1 |a Jacobs, Eastman N.  |q (Eastman Nixon),  |d 1902-1987. 
700 1 |a Jones, Robert T.  |q (Robert Thomas),  |d 1910-1999. 
700 1 |a Kaplan, Carl. 
700 1 |a Katzoff, S.  |q (Samuel),  |d 1909- 
700 1 |a Kuhn, Paul. 
700 1 |a Lindsey, W. F. 
700 1 |a Osgood, William R. 
700 1 |a Pearson, Henry A.  |q (Henry Adolph),  |d 1906- 
700 1 |a Pinkel, Benjamin,  |d 1909- 
700 1 |a Pinkerton, Robert M. 
700 1 |a Rhode, Richard V. 
700 1 |a Rothrock, A. M.  |q (Addison May),  |d 1903-1971. 
700 1 |a Selden, Robert F. 
700 1 |a Silverstein, Abe. 
700 1 |a Soule, Hartley A.  |q (Hartley Akin),  |d 1904-1988. 
700 1 |a Spencer, Robert C.  |q (Robert Champlin),  |d 1926- 
700 1 |a Voss, Fred. 
700 1 |a Wenzinger, Carl J.  |q (Carl Joseph),  |d 1903-1988. 
700 1 |a Wetmore, J. W.  |q (Joseph W.) 
710 1 |a United States.  |b National Advisory Committee for Aeronautics. 
830 0 |a Senate document (United States. Congress. Senate) ;  |v 76th Congress, no. 3. 
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