NACA Digital Library - UK Mirror

    80 records

  1. Weick, Fred E Scudder, Nathan F; The effect on lift, drag, and spinning characteristics of sharp leading edges on airplane wings; naca-tn-447; February 1933

  2. Defrance, Smith J; The aerodynamic effect of a retractable landing gear; naca-tn-456; March 1933

  3. Heald, R H (Bureau of Standards); Rolling, yawing, and hinge moments produced by rectangular ailerons; naca-tn-441; 1933

  4. Schubauer, G B (Bureau of Standards); Jet propulsion with special reference to thrust augmenters; naca-tn-442; 1933

  5. Weick, Fred E Wenzinger, Carl J; Wind tunnel research concerning lateral control devices, particularly at high angles of attack VII : Handley Page tip and full-span slots with ailerons and spoilers; naca-tn-443; 1933

  6. Burke, Walter F (University of Michigan); Working charts for the stress analysis of elliptic rings; naca-tn-444; 1933

  7. Weick, Fred E Shortal, Joseph A; Wind tunnel research comparing lateral control devices, particularly at high angles of attack VIII : straight and skewed ailerons on wings with rounded tips; naca-tn-445; February 1933

  8. Heald, R H (Bureau of Standards); Effect of aileron displacement on wing characteristics; naca-tn-448; February 1933

  9. Weick, Fred E Wenzinger, Carl J; Wind-tunnel research comparing lateral control devices, particularly at high angles of attack IX : tapered wings with ordinary ailerons; naca-tn-449; February 1933

  10. Wilkie, J B (Bureau of Standards); Mercerization of cotton for strength with special reference to aircraft cloth; naca-tn-450; February 1933

  11. Weick, Fred E Noyes, Richard W; Wind tunnel research comparing lateral control devices, particularly at high angles of attack X : various control devices on a wing with a fixed auxiliary airfoil; naca-tn-451; March 1933

  12. Lesley, E P (Stanford University); Experiments with a counter-propeller; naca-tn-453; March 1933

  13. Spanogle, J A Buckley, E C; The N.A.C.A. combustion chamber gas-sampling valve and some preliminary test results; naca-tn-454; March 1933

  14. Lundquist, Eugene E; Comparison of three methods for calculating the compressive strength of flat and slightly curved sheet and stiffener combinations; naca-tn-455; March 1933

  15. HOCKER RAY W; The aerodynamic characteristics of airfoils as affected by surface roughness; naca-tn-457; April 1933

  16. Weick, Fred E Harris, Thomas A; Wind tunnel research comparing lateral control devices, particularly at high angles of attack XI : various floating tip ailerons on both rectangular and tapered wings; naca-tn-458; May 1933

  17. Weick, Fred E Platt, Robert C; Wind-tunnel tests on model wing with Fowler flap and specially developed leading-edge slot; naca-tn-459; May 1933

  18. Hood, Manley J White, James A; Full-scale wind-tunnel research on tail buffeting and wing-fuselage interference of a low-wing monoplane; naca-tn-460; May 1933

  19. Dearborn, Clinton H; The effect of rivet heads on the characteristics of a 6 by 36 foot Clark Y metal airfoil; naca-tn-461; May 1933

  20. Miller, Roy A (Consolidated Aircraft Corporation) Wood, Karl D (Cornell University); Formulas for the stress analysis of circular rings in a monocoque fuselage; naca-tn-462; June 1933

  21. Weick, Fred E Sanders, Robert; Aerodynamic tests of a low aspect ratio tapered wing with various flaps, for use on tailless airplanes; naca-tn-463; June 1933

  22. Shoemaker, James M Parkinson, John B; A complete tank test of a model of a flying-boat hull-N.A.C.A. Model No.11; naca-tn-464; July 1933

  23. Marsh, E T Waldron, C D; Some characteristics of sprays obtained from pintle-type injection models; naca-tn-465; July 1933

  24. Schey, Oscar W Young, Alfred W; Engine performance with a hydrogenated safety fuel; naca-tn-466; July 1933

  25. Scudder, Nathan F; A study of factors affecting the steady spin of an airplane; naca-tn-468; August 1933

  26. Kuhn, Paul; A summary of design formulas for beams having thin webs in diagonal tension; naca-tn-469; August 1933

  27. Parkinson, John B; A complete tank test of a model of a flying-boat Hull - N.A.C.A. model no.11-A; naca-tn-470; September 1933

  28. Shoemaker, James H; A complete tank test of a model of flying-boat Hull - N.A.C.A. Model 16; naca-tn-471; September 1933

  29. Wenzinger, Carl J; The effect of partial-span split flaps on the aerodynamic characteristics of a Clark Y wing; naca-tn-472; September 1933

  30. Bell, Joe W; Tank tests of two floats for high-speed seaplanes; naca-tn-473; November 1933

  31. Bamber, M J Zimmerman, C H; Effect of stabilizer location upon pitching and yawing moments in spins as shown by tests with the spinning balance; naca-tn-474; November 1933

  32. Wallace, Rudolf, N; The effect of split trailing-edge wing flaps on the aerodynamic characteristics of a parasol monoplane; naca-tn-475; November 1933

  33. Garlock, E A (Bureau of Standards) Ellis, Greer (Bureau of Standards); The effect on engine performance of change in jacket-water outlet temperature; naca-tn-476; November 1933

  34. Sanders, Robert; Aerodynamic tests of a low aspect ratio tapered wing with an auxiliary airfoil for use on tailless airplanes; naca-tn-477; November 1933

  35. Soule, Hartley A Wetmore, J W; The effects of slots and flaps on lateral control of a low-wing monoplane as determined in flight; naca-tn-478; November 1933

  36. Lundquist, Eugene E; Strength tests of thin-walled duralumin cylinders in pure bending; naca-tn-479; December 1933

  37. Jacobs, Eastman N; The drag of streamline wires; naca-tn-480; December 1933

  38. Jacobs, Eastman N; The reduction in drag of a forward-sloping windshield; naca-tn-481; December 1933

  39. Dawson, John R; The effect of spray strips on a model of the P3M-1 flying boat hull; naca-tn-482; December 1933

  40. Anderson, Raymond F; Charts for determining the pitching moment of tapered wings with sweepback and twist; naca-tn-483; December 1933

  41. Rothrock, A M; Combustion in a high-speed compression-ignition engine; naca-report-401; 1933

  42. Gelalles, A G; Effect of orifice length-diameter ratio on fuel sprays for compression-ignition engines; naca-report-402; 1933

  43. Theodorsen, Theodore Clay, William C; Ice prevention on aircraft by means of engine exhaust heat and a technical study of heat transmission from a Clark y airfoil; naca-report-403; 1933

  44. Schey, Oscar W Rollin, Vern G; The effect of increased carburetor pressure on engine performance at several compression ratios; naca-report-404; 1933

  45. Upson, Ralph H Klikoff, W A; Application of practical hydrodynamics to airship design; naca-report-405; 1933

  46. Peck, W D Beard, A P; Drop and flight tests on NY-2 landing gears including measurements of vertical velocities at landing; naca-report-406; 1933

  47. Weick, Fred E Wenzinger, Carl J; The characteristics of a Clark y wing model equipped with several forms of low-drag fixed slots; naca-report-407; 1933

  48. Oswald, W Bailey; General formulas and charts for the calculation of airplane performance; naca-report-408; 1933

  49. Theodorsen, Theodore Freeman, Ira M; The elimination of fire hazard due to back fires; naca-report-409; 1933

  50. Theodorsen, Theodore; The theory of wind-tunnel wall interference; naca-report-410; 1933

  51. Theodorsen, Theodore; Theory of wing sections of arbitrary shape; naca-report-411; 1933

  52. Harris, Thomas A; The 7 by 10 foot wind tunnel of the National Advisory Committee for Aeronautics; naca-report-412; 1933

  53. Rhode, Richard V Pearson, Henry A; A method for computing leading-edge loads; naca-report-413; 1933

  54. Mcavoy, William H Schey, Oscar W Young, Alfred W; The effect on airplane performance of the factors that must be considered in applying low-drag cowling to radial engines; naca-report-414; 1933

  55. Wood, Donald H; Tests of nacelle-propeller combinations in various positions with reference to wings. Part I : thick wing-N.A.C.A. cowled nacelle-tractor propeller; naca-report-415; 1933

  56. Jacobs, Eastman N Abbott, Ira H; The NACA variable-density wind tunnel; naca-report-416; 1933

  57. Noyes, Richard W; Pressure distribution tests on a series of Clark y biplane cellules with special reference to stability; naca-report-417; 1933

  58. Weick, Fred E; Preliminary investigation of modifications to conventional airplanes to give nonstalling and short-landing characteristics; naca-report-418; 1933

  59. Weick, Fred E Wenzinger, Carl J; Wind-tunnel research comparing lateral control devices, particularly at high angles of attack I : ordinary ailerons on rectangular wings; naca-report-419; 1933

  60. Beij, K Hilding; Aircraft speed instruments; naca-report-420; 1933

  61. Stickle, George W; Measurement of the differential and total thrust and torque of six full-scale adjustable-pitch propellers; naca-report-421; 1933

  62. Weick, Fred E Noyes, Richard W; Wind-tunnel research comparing lateral control devices, particularly at high angles of attack II : slotted ailerons and frise ailerons; naca-report-422; 1933

  63. Weick, Fred E Wenzinger, Carl J; Wind-tunnel research comparing lateral control devices, particularly at high angles of attack III : ordinary ailerons rigged up 10 degrees when neutral; naca-report-423; 1933

  64. Weick, Fred E Harris, Thomas A; Wind-tunnel research comparing lateral control devices, particularly at high angles of attack IV : floating tip ailerons on rectangular wings; naca-report-424; 1933

  65. Lee, Dana W; The effect of nozzle design and operating conditions on the atomization and distribution of fuel sprays; naca-report-425; 1933

  66. Brooks, D G Garlock, E A; The effect of humidity on engine power at altitude; naca-report-426; 1933

  67. Weick, Fred E Shortal, Joseph A; The effect of multiple fixed slots and a trailing-edge flap on the lift and drag of a Clark Y airfoil; naca-report-427; 1933

  68. Weick, Fred E Bamber, Millard J; Wind-tunnel tests of a Clark Y wing with a narrow auxiliary airfoil in different positions; naca-report-428; 1933

  69. Rothrock, A M; The NACA apparatus for studying the formation and combustion of fuel sprays and the results from preliminary tests; naca-report-429; 1933

  70. Freeman, Hugh B; Measurements of flow in the boundary layer of a 1/40-scale model of the U. S. Airship "Akron."; naca-report-430; 1933

  71. Zimmerman, C H; Characteristics of Clark Y airfoils of small aspect ratios; naca-report-431; 1933

  72. Freeman, Hugh B; Force measurements on a 1/40-scale model of the U. S. Airship "Akron."; naca-report-432; 1933

  73. Gelalles, A G Marsh, E T; Rates of fuel discharge as affected by the design of fuel-injection systems for internal-combustion engines; naca-report-433; 1933

  74. Wheatley, John B; Lift and drag characteristics and gliding performance of an autogiro as determined in flight; naca-report-434; 1933

  75. Rothrock, A M Waldron, C D; Fuel vaporization and its effect on combustion in a high-speed compression-ignition engine; naca-report-435; 1933

  76. Dryden, Hugh L Monish, B H; The effect of area aspect ratio on the yawing moments of rudders at large angles of pitch on three fuselages; naca-report-437; 1933

  77. Lee, Dana W; Experiments on the distribution of fuel in fuel sprays; naca-report-438; 1933

  78. Weick, Fred E Shortal, Joseph A; Wind-tunnel research comparing lateral control devices, particularly at high angles of attack V : spoilers and ailerons on rectangular wings; naca-report-439; 1933

  79. Castleman, R A , Jr; The mechanism of atomization accompanying solid injection; naca-report-440; 1933

  80. Jacobs, Eastman N Ward, Kenneth E Pinkerton, Robert M; The characteristics of 78 related airfoil sections from tests in the variable-density wind tunnel; naca-report-460; 1933

Last Updated: December 9, 2006, 12:07 pm
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