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Ames, Milton B. [Other]; Bailey, F.J [Other]; Biermann, Arnold E. [Other]; Brevoort, Maurice J. [Other]; Bullivant, W. Kenneth [Other]; Cohen, Doris [Other]; Crigler, John L. [Other]; Dutee, Francis J. [Other]; Ellenbrock, Herman H. [Other]; Gilruth, Robert Rowe [Other]; Gracey, William [Other]; Harris, Thomas A. [Other]; House, Rufus O. [Other]; Jones, Robert Thomas [Other]; Joyner, Upshur T. [Other]; Lowry, John G. [Other]; Miller, Cearcy D. [Other]; Naiman, Irven [Other]; Recant, Isidore G. [Other]; Rothrock, A.M [Other]; Wallace, Arthur R. [Other]; Waldron, C.D [Other]; Wenzinger, Carl J. [Other]; Rogallo, Francis M. [Other]; [...] ; United States Congress Senate, United States Dept. of Commerce National Bureau of Standards (1913-1988), United States National Advisory Committee for Aeronautics

Twenty-seventh annual report of the National Advisory Committee for Aeronautics, 1941, including Technical Reports Nos. 704 to 726

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  • Media type: E-Book
  • Title: Twenty-seventh annual report of the National Advisory Committee for Aeronautics, 1941, including Technical Reports Nos. 704 to 726
  • Contributor: Ames, Milton B. [Other]; Bailey, F.J. [Other]; Biermann, Arnold E. [Other]; Brevoort, Maurice J. [Other]; Bullivant, W. Kenneth [Other]; Cohen, Doris [Other]; Crigler, John L. [Other]; Dutee, Francis J. [Other]; Ellenbrock, Herman H. [Other]; Gilruth, Robert Rowe [Other]; Gracey, William [Other]; Harris, Thomas A. [Other]; House, Rufus O. [Other]; Jones, Robert Thomas [Other]; Joyner, Upshur T. [Other]; Lowry, John G. [Other]; Miller, Cearcy D. [Other]; Naiman, Irven [Other]; Recant, Isidore G. [Other]; Rothrock, A.M. [Other]; Wallace, Arthur R. [Other]; Waldron, C.D. [Other]; Wenzinger, Carl J. [Other]; Rogallo, Francis M. [Other]; Roop, Frederick C. [Other]; Stickle, George M. [Other]; White, M.D. [Other]; Sears, Richard I. [Other]; Spencer, Robert C. [Other]; Turner, W.N. [Other]
  • Corporation: United States, Dept. of Commerce, National Bureau of Standards (1913-1988) ; United States, National Advisory Committee for Aeronautics
  • Published: Washington, DC, 1942
    Online-Ausg., Chester, Vt: NewsBank, inc, 2008
  • Published in: United States congressional serial set ; serial set no. 10678
    Senate document / 77th Congress, 2nd session. Senate ; no. 170
  • Extent: Online-Ressource (433 p); illustrations, tables
  • Language: English
  • Reproduction series: U.S. Congressional Serial Set, 1817-1980
  • Type of reproduction: Online-Ausg.
  • Place of reproduction: Chester, Vt: NewsBank, inc, 2008
  • Origination:
  • Footnote: A graphical method of determining pressure distribution in two-dimensional flow, by Robert T. Jones and Doris Cohen, N.A.C.A. [No. 722], p. 313
    A high-speed motion-picture study of normal combustion, knock, and preignition in a spark-ignition engine, by A.M. Rothrock, R.C. Spencer, and Cearcy D. Miller, N.A.C.A. [No. 704], p. 15
    A simplified theoretical method of determining the characteristics of a lifting rotor in forward flight, by F.J. Bailey, Jr., N.A.C.A. [No. 716], p. 209
    An analysis of the stability of an airplane with free controls, by Robert T. Jones and Doris Cohen, N.A.C.A. [No. 709], p. 109
    An apparatus for measuring rates of discharge of a fuel-injection system, by Francis J. Dutee, N.A.C.A. [No. 714], p. 193
    Analysis and prediction of longitudinal stability of airplanes, by R.R. Gilruth and M.D. White, N.A.C.A. [No. 711], p. 137
    Appendix, p. 118
    Determination of control-surface characteristics from NACA plain-flap and tab data, by Milton B. Ames, Jr. and Richards I. Sears, N.A.C.A. [No. 721], p. 295
    Effect of aging on mechanical properties of aluminum-alloy rivets, by Frederick C. Roop, National Bureau of Standards [No. 724], p. 353
    Effect of body nose shape on the propulsive efficiency of a propeller, by G.W. Stickle, John L. Crigler, and Irven Naiman, N.A.C.A. [No. 725], p. 371
    Flow coefficients of monosleeve valves, by C.D. Waldron, N.A.C.A. [No. 717], p. 227
    Internal-flow systems for aircraft, by F.M. Rogallo, N.A.C.A. [No. 713], p. 165
    Lateral control required for satisfactory flying qualities based on flight tests of numerous airplanes, by R.R. Gilruth and W.N. Turner, N.A.C.A. [No. 715], p. 201
    Preignition characteristics of several fuels under simulated engine conditions, by R.C. Spencer, N.A.C.A. [No. 710], p. 121
    Pressure available for cooling with cowling flaps and tab data, by George W. Stickle, Irven Naiman, and John L. Crigler, N.A.C.A. [No. 720], p. 283
    Pressure distribution over an NACA 23021 airfoil with a slotted and a split flap, by Thomas A. Harris and John G. Lowry, N.A.C.A. [No. 718], p. 241
    Propeller analysis from experimental data, by George M. Stickle and John L. Crigler, N.A.C.A. [No. 712], p. 147
    Tests of the NACA 0025 and 0035 airfoils in the full-scale wind tunnel, by W. Kenneth Bullivant, N.A.C.A. [No. 708], p. 91
    The additional-mass effect of plates as determined by experiments, by William Gracey, N.A.C.A. [No. 707], p. 81
    The design of fins for air-cooled cylinders, by Arnold E. Biermann and Herman H. Ellerbrock, Jr. [No. 726], p. 401
    The problem of cooling an air-cooled cylinder on an aircraft engine, by M.J. Brevoort and U.T. Joyner, N.A.C.A. [No. 719], p. 267
    Wind-tunnel investigation of NACA 23012, 23021, and 23030 airfoils equipped with 40-percent-chord double-slotted flaps, by Thomas A. Harris and Isidore G. Recant, N.A.C.A. [No. 723], p. 321
    Wind-tunnel investigation of effect of interference on lateral-stability characteristics of four NACA 23012 wings, an elliptical and a circular fuselage, and vertical fins, by Rufus O. House and Arthur R. Wallace, N.A.C.A. [No. 705], p. 31
    Wind-tunnel investigation of spoiler deflector, and slot lateral-control devices on wings with full-span split and slotted flaps, by Carl J. Wenzinger and Francis M. Rogallo, N.A.C.A. [No. 706], p. 51
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