NACA Digital Library - UK Mirror
109 records
- Levy, Samuel (National Bureau of Standards) Krupen, Philip (National Bureau of Standards); Large-deflection theory for end compression of long rectangular plates rigidly clamped along two edges; naca-tn-884; 1943
- W. D. Kroll; Tables of stiffness and carry-over factor for flat rectangular plates under compression; naca-arr-3k27; November, 1943
- W. D. Kroll, Gordon P. Fisher, George J. Heimrel; Charts for calculation of the critical stress for local instability of columns with I-, Z-, channel and rectangular-tube section; naca-arr-3k04; November, 1943
- Eugene E. Lundquist, Elbridge Z. Stowell, Evan H. Schuette; Principles of moment distribution applied to stability of structures composed of bars or plates; naca-arr-3k06; November 1943
- Ribner, Herbert S; Propellers in yaw; naca-report-820; December 1943
- Seliger, Victor (Lockheed Aircraft Corporation); Effect of rivet pitch upon the fatigue strength of single-row riveted joints of 0.025- to 0.025-inch 24S-T alclad; naca-tn-900; July 1943
- Moore, R L (Aluminum Company of America) Wescoat, C (Aluminum Company of America); Bearing strengths of some wrought-aluminum alloys; naca-tn-901; August 1943
- Lundquist, Eugene E Rossman, Carl A Houbolt, John C; A method for determining the column curve from tests of columns with equal restraints against rotation on the ends; naca-tn-903; August 1943
- Sherwood, A W (University of Maryland); The strength of thin-wall cylinders of D cross section in combined pure bending and torsion; naca-tn-904; September 1943
- (Author(s) Not Available); Some investigations of the general instability of stiffened metal cylinders I : review of theory and bibliography; naca-tn-905; 1943
- (Author(s) Not Available); Some investigations of the general instability of stiffened metal cylinders II : preliminary tests of wire-braced specimens and theoretical studies; naca-tn-906; 1943
- (Author(s) Not Available); Some investigations of the general instability of stiffened metal cylinders III : continuation of tests of wire-braced specimens and preliminary tests of sheet-covered specimens; naca-tn-907; 1943
- (Author(s) Not Available); Some investigations of the general instability of stiffened metal cylinders IV : continuation of tests of sheet-covered specimens and studies of the buckling phenomena of unstiffened circular cylinders; naca-tn-908; 1943
- (Author(s) Not Available); Some investigations of the general instability of stiffened metal cylinders VII : stiffened metal cylinders subjected to combined bending and torsion; naca-tn-911; November 1943
- Aitchison, C S (National Bureau of Standards) Miller, James A (National Bureau of Standards); A subpress for compressive tests; naca-tn-912; December 1943
- Aitchison, C S (National Bureau of Standards) Miller, James A (National Bureau of Standards); Tensile and compressive tests of magnesium alloy J-1 sheet; naca-tn-913; December 1943
- Dolan, Thomas J (University of Illinois); Certain mechanical strength properties of aluminum alloys 25S-T and X76S-T; naca-tn-914; October 1943
- Livengood, James C (Massachusetts Institute of Technology) Stanitz, John D (Massachusetts Institute of Technology); The effect of inlet-valve design, size, and lift on the air capacity and output of a four-stroke engine; naca-tn-915; November 1943
- Sharp, W H (Aluminum Company of America); The effect of the type of specimen on the shear strengths of driven rivets; naca-tn-916; November 1943
- Donnell, L H (Chance Vought Aircraft); The stability of isotropic or orthotopic cylinders or flat or curved panels, between and across stiffeners, with any edge conditions between hinged and fixed, under any combination of compression and shear; naca-tn-918; December 1943
- Rogowski, A R (Massachusetts Institute of Technology) Taylor, C Fayette (Massachusetts Institute of Technology); Part-throttle operation and control of a piston-ported two-stroke cylinder; naca-tn-919; November 1943
- Scott, Merit (Pennsylvania State College, State College, PA) Weber, Robert L (Pennsylvania State College, State College, PA); Requirements for auxiliary stiffeners attached to panels under combined compression and shear; naca-tn-921; September 16, 1943
- Kynoch, William (University of Michigan, Ann Arbor, Mich) Patronsky, L A (University of Michigan, Ann Arbor, Mich); Effect of fillers and of mixing procedure on the strength of plastic materials; naca-tn-878; 1943
- Moore, R L (Aluminum Company of America, New Kensington, Penna); Torsional strength of aluminum-alloy round tubing; naca-tn-879; 1943
- Weske, John R (Case School of Applied Science); Methods of measurement of high air velocities by the hot-wire method; naca-tn-880; February 1943
- Weske, John R (Case School of Applied Science); A hot-wire circuit with very small time lag; naca-tn-881; February 1943
- Niles, Alfred S (Stanford University, Calif); Tests of flat panels with four types of stiffeners; naca-tn-882; 1943
- Holt, Marshall (Aluminum Company of America); Tests of aluminum-alloy stiffened-sheet specimens cut from an airplane wing; naca-tn-883; 1943
- Moore, R L (Aluminum Company of America) Paul, D A (Aluminum Company of America); Torsion tests of 24S-T aluminum-alloy noncircular bar and tubing; naca-tn-885; 1943
- Mebs, R W (National Bureau of Standards) Mcadam, D J , Jr (National Bureau of Standards); Torsional elastic properties of 18:8 chromium-nickel steel as affected by plastic deformation and by heat treatment; naca-tn-886; 1943
- Mcpherson, Albert E (National Bureau of Standards); A portable calibrator for dynamic strain gages; naca-tn-887; February 1943
- Hill, H N (Aluminum Company of America); Torsion of flanged members with cross sections restrained against warping; naca-tn-888; March 1943
- Kies, J A (National Bureau of Standards) Holshouser, W L (National Bureau of Standards); Effects of prior fatigue-stressing of the impact resistance of chromium-molybdenum aircraft steel; naca-tn-889; March 1943
- Delano, James B; Pressure distribution on the fuselage of a midwing airplane model at high speeds; naca-tn-890; February 1943
- Shih-I, Pai (California Institute of Technology); Turbulent flow between rotating cylinders; naca-tn-892; March 1943
- Hildebrand, Francis B (Massachusetts Institute of Technology) Reissner, Eric (Massachusetts Institute of Technology); Least-work analysis of the problem of shear lag in box beams; naca-tn-893; 1943
- Hildebrand, Francis B (Massachusetts Institute of Technology, Cambridge, Mass); The exact solution of shear-lag problems in flat panels and box beams assumed rigid in the transverse direction; naca-tn-894; 1943
- Levy, Samuel (National Bureau of Standards); Large-deflection theory of curved sheet; naca-tn-895; May 1943
- Osgood, William R (National Bureau of Standards); Round heat-treated chromium-molybdenum-steel tubing under combined loads; naca-tn-896; July 1943
- Sharp, W H (Aluminum Company of America) Moore, R L (Aluminum Company of America); Bearing tests of magnesium-alloy sheet; naca-tn-897; June 1943
- Mcpherson, A E (National Bureau of Standards); Adaptor for measuring principal strains with Tuckerman strain gage; naca-tn-898; 1943
- Holt, M (Aluminum Company of America); Column strength of magnesium alloy AM-57S; naca-tn-899; July 1943
- Russell, H W (Battelle Memorial Institute) Gillett, H W (Battelle Memorial Institute) Jackson, L R (Battelle Memorial Institute) Foley, G M (Battelle Memorial Institute); The effect of surface finish on the fatigue performance of certain propeller materials; naca-tn-917; December 1943
- Moore, R L (Aluminum Company of America) Wescoat, C (Aluminum Company of America); Bearing strengths of bare and alclad XA75S-T and 24S-T81 aluminum alloy sheet; naca-tn-920; December 1943
- Charters, Alex C , Jr (California Institute of Technology); Transition between laminar and turbulent flow by transverse contamination; naca-tn-891; March 1943
- (Author(s) Not Available); Some investigations of the general instability of stiffened metal cylinders VI : stiffened metal cylinders subjected to combined bending and transverse shear; naca-tn-910; 1943
- Kaplan, Carl; On a new method for calculating the potential flow past a body of revolution; naca-report-752; 1943
- Olson, Roland E Land, Norman S; Methods used in the NACA tank for the investigation of the longitudinal-stability characteristics of models of flying boats; naca-report-753; 1943
- Sanders, J C Wilsted, H D Mulcahy, B A; Operating temperatures of a sodium-cooled exhaust valve as measured by a thermocouple; naca-report-754; 1943
- Gilruth, R R; Requirements for satisfactory flying qualities of airplanes; naca-report-755; 1943
- Rothrock, Addison M Krsek, Alois, Jr Jones, Anthony W; The induction of water to the inlet air as a means of internal cooling in aircraft-engine cylinders; naca-report-756; 1943
- Gerrish, Harold C Meem, J Lawrence, Jr; The measurement of fuel-air ratio by analysis for the oxidized exhaust gas; naca-report-757; 1943
- Sinnette, John T Schey, Oscar W King, J Austin; Performance of NACA eight-stage axial-flow compressor designed on the basis of airfoil theory; naca-report-758; 1943
- Pearson, Henry A; Derivation of charts for determining the horizontal tail load variation with any elevator motion; naca-report-759; 1943
- Sanders, Newell D; A method of estimating the knock rating of hydrocarbon fuel blend; naca-report-760; 1943
- Miller, Cearcy D Olsen, H Lowell; Identification of knock in NACA high-speed photographs of combustion in a spark-ignition engine; naca-report-761; 1943
- Greenberg, Harry Sternfield, Leonard; A theoretical investigation of the lateral oscillations of an airplane with free rudder with special reference to the effect of friction; naca-report-762; 1943
- Stack, John; Tests of airfoils designed to delay the compressibility burble; naca-report-763; 1943
- Allen, H Julian Look, Bonne C; A method for calculating heat transfer in the laminar flow region of bodies; naca-report-764; 1943
- Parkinson, John B Olson, Roland E Draley, Eugene C Luoma, Arvo A; Aerodynamic and hydrodynamic tests of a family of models of flying hulls derived from a streamline body -- NACA model 84 series; naca-report-766; 1943
- Hood, Manley J Allen, H Julian; The problem of longitudinal stability and control at high speeds; naca-report-767; 1943
- Kaplan, Carl; The flow of a compressible fluid past a curved surface; naca-report-768; 1943
- Campbell, John P Seacord, Charles L , Jr; The effect of mass distribution on the lateral stability and control characteristics of an airplane as determined by tests of a model in the free-flight tunnel; naca-report-769; 1943
- Swanson, Robert S Toll, Thomas A; Jet-boundary corrections for reflection-plane models in rectangular wind tunnel; naca-report-770; 1943
- Johnston, J Ford; Review of flight tests of NACA C and D cowlings on the XP-42 airplane; naca-report-771; 1943
- Von Doenhoff, Albert E Tetervin, Neal; Determination of general relations for the behavior of turbulent boundary layers; naca-report-772; 1943
- Becker, John V Baals, Donald D; Analysis of heat and compressibility effects in internal flow systems and high-speed tests of a ram-jet system; naca-report-773; 1943
- Lowry, John G; Resume of hinge-moment data for unshielded horn- balanced control surfaces; naca-wr-l-169; June 1943
- Purser, Paul E; Wind-tunnel investigation of control-surface characteristics XIV : NACA 0009 airfoil with a 20-percent-chord double plain flap; naca-wr-l-290; June 1943
- Ribner, Herbert S; Proposal for a propeller side-force factor; naca-wr-l-336; December 1943
- Schuldenfrei, Marvin; Some notes on the determination of the stick-fixed neutral point from wind-tunnel data; naca-wr-l-344; September 1943
- Anderson, R A; Wind tunnel tests of ailerons at various speeds IV : ailerons of 0.20 airfoil chord and true contour with 0.35 aileron-chord extreme blunt-nose balance on the NACA 23012 airfoil; naca-wr-l-433; August 1943
- Denaci, H G; Wind tunnel tests of ailerons at various speeds V : pressure distributions over the NACA 66,2-216 and NACA 23012 airfoils with various balances on 0.20-chord ailerons; naca-wr-l-434; November 1943
- Crandall, Stewart M; Wind-tunnel investigation of trimming tabs on a thickened and beveled aileron on a tapered low-drag wing; naca-wr-l-435; March 1943
- Nelson, W J; Wind tunnel investigation of rear underslung fuselage ducts; naca-wr-l-438; September 1943
- Dingeldein, Richard C; Full-scale tunnel investigation of the pressure distribution over the tail of the P-47B airplane; naca-wr-l-439; May 1943
- Hoggard, H Page; Wind tunnel investigation of control-surface characteristics XI : various large overhang and internal-type aerodynamic balances for a straight- contour flap on the NACA 0015 airfoil; naca-wr-l-447; 1943
- Tetervin, Neal; Tests in the NACA two-dimensional low-turbulence tunnel of airfoil sections designed to have small pitching moments and high lift-drag ratios; naca-wr-l-452; September 1943
- Toll, Thomas A; Jet-boundary corrections for reflection-plane models in rectangular wind tunnels; naca-wr-l-458; May 1943
- Turner, Thomas R; Wind-tunnel investigation of effect of yaw on lateral-stability characteristics V : symmetrically tapered wing with a circular fuselage having a horizontal and a vertical tail; naca-wr-l-459; June 1943
- Gelbart, Abe; On a function-theory method for obtaining potential-flow patterns of a compressible fluid; naca-wr-l-460; July 1943
- Schuette, Evan H; Critical stresses for plates; naca-wr-l-466; October 1943
- Riebe, John M; Wind-tunnel investigation of an NACA 23012 airfoil with a 0.30-airfoil-chord double slotted flap; naca-wr-l-469; December 1943
- Moggio, Edwin M; The longitudinal shear strength required in double-angle columns of 24S-T aluminum alloy; naca-wr-l-472; May 1943
- Hastings, Charles E; NACA radio ground-speed system for aircraft; naca-wr-l-477; February 1943
- Draper, John W; Free-flight-tunnel investigation of the effect of the fuselage length and the aspect ratio and size of the vertical tail on lateral stability and control; naca-wr-l-487; April 1943
- Mendelsohn, Robert A; Wind-tunnel tests of a piston-type control booster on an airfoil and aileron model; naca-wr-l-494; November 1943
- Crate, Harold; A preliminary study of machine-countersunk flush rivets subjected to a combined static and alternating shear load; naca-wr-l-495; December 1943
- Mattson, Axel T; The effect of spinner-body gap on the pressures available for cooling in the NACA E-type cowling; naca-wr-l-497; March 1943
- Mckinney, Marion O , Jr; Flight tests of a glider model towed by twin parallel towlines; naca-wr-l-498; April 1943
- Levin, L Ross; Tests of 10-inch 24S-T aluminum-alloy shear panels with 1-1/2-inch holes I; naca-wr-l-500; June 1943
- Pitkin, Marvin; Effect of wing leading-edge slots on the spin and recovery characteristics of airplanes; naca-wr-l-504; April 1943
- Fischel, Jack; Wind-tunnel investigation of a full-span retractable flap in combination with full-span plain and internally balanced ailerons on a tapered wing; naca-wr-l-506; August 1943
- Benson, James M; Hydrodynamic-stability tests of a model of a flying boat and of a planing surface having a small downward projection (hook) on the planing bottom near the step; naca-wr-l-518; 1943
- Schuette, Evan H; Test data on the shear strength of joints assembled with round-head and brazier-head rivets; naca-wr-l-519; June 1943
- Seacord, Charles L , Jr; Effect of wing loading and altitude on lateral stability and control characteristics of an airplane as determined by tests of a model in the free-flight tunnel; naca-wr-l-522; June 1943
- Mckee, John W; Wind-tunnel investigation of a plain aileron with thickened and beveled trailing edges on a tapered low-drag wing; naca-wr-l-526; 1943
- Houbolt, John C; A preliminary study of the effect of compressive load on the fairness of a low-drag wing specimen with Z-section stiffeners; naca-wr-l-527; 1943
- Braslow, Albert L; Investigation of surface irregularities on an NACA 63(420)-416, a=1.0 airfoil section for the Glenn L. Martin Company design 195; naca-wr-l-534; October 1943
- Dow, Norris F; The analysis of strains indicated by multiple-strand resistance-type wire strain gages used as rosettes; naca-wr-l-536; 1943
- Ritchie, Virgil S; A simplified chart for determining Mach number and true airspeed from airspeed-indicator readings; naca-wr-l-473; March 1943
- Hoggard, H. Page, Jr.; Wind tunnel investigation of control surface characteristics XII : various cover-plate alinements on the NACA 0015 airfoil with a 30 percent chord flap and large sealed internal balance; naca-wr-l-511; 1943
- Sears, Richard I.; Wind-tunnel data on the aerodynamic characteristics of airplane control surfaces; naca-wr-l-663; 1943
- Purser, Paul E., Riebe, John M.; Wind-tunnel investigation of control-surface characteristics XV : various contour modifications of a 0.30-airfoil-chord plain flap on an NACA 66(215)-014 airfoil; naca-wr-l-668; 1943
- Gillis, Clarence L, Lockwood, Vernard E; Wind-tunnel investigation of control-surface characteristics XIII : various flap overhangs used with a 30-percent-chord flap in an NACA 66-009 airfoil; naca-wr-l-314; 1943
- Letko, W, Denaci, H G, Freed, C; Wind tunnel tests of ailerons at various speeds I : ailerons of 0.20 airfoil chord and true contour with 0.35 aileron-chord extreme blunt nose balance on the NACA 66,2-216 airfoil; naca-wr-l-431; 1943
- Denaci, H G, Bird, J D; Wind-tunnel tests of ailerons at various speeds II : ailerons of 0.20 airfoil chord and true contour with 0.60 aileron-chord sealed internal balance on the NACA 66,2-216 airfoil; naca-wr-l-432; 1943
- Vogeley, A W; Flight measurements of compressibility effects on a three-blade thin Clark Y propeller operating at constant advance-diameter ratio and blade angle; naca-wr-l-505; 1943
- Guggenheim Aeronautical Laboratory; Some Investigations of the General Instability of Stiffened Metal Cylinders V - Stiffened Metal Cylinders Subjected to Pure Bending; naca-tn-909; August 1943
Last Updated: December 9, 2006, 12:07 pm
Administrator: Paul A S Needham