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41 reports
Analytical Investigation of Icing Limit for Diamond-Shaped Airfoil in Transonic and Supersonic Flow
Author(s): Callaghan, Edmund E. Corporate Author: National Advisory Committee for Aeronautics Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1953-01 Report Number: NACA TN 2861
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A Method for Rapid Determination of the Icing Limit of a Body in Terms of the Stream Conditions
Author(s): Callaghan, Edmund E. Corporate Author: Lewis Flight Propulsion Laboratory Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1953-03 Report Number: NACA TN 2914
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Steady Vibrations of Wing of Circular Plan Form (p. 1-50)
Author(s): Kochin, N. E. Corporate Author: National Advisory Committee for Aeronautics Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1953-01 Report Number: NACA TM 1324
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Steady Vibrations of Wing of Circular Plan Form (p. 51-93)
Author(s): Kochin, N. E. Corporate Author: National Advisory Committee for Aeronautics Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1953-01 Report Number: NACA TM 1324
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Reflection of a Weak Shock Wave from a Boundary Layer Along a Flat Plate. I. Interaction of Weak Shock Waves with Laminar and Turbulent Boundary Layers Analyzed by Momentum-Integral Method
Author(s): Ritter, Alfred Corporate Author: Cornell University Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1953-01-27 Report Number: NACA TN 2868
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A Digital Automatic Multiple Pressure Recorder
Author(s): Coss, Bert A. Corporate Author: Lewis Flight Propulsion Laboratory Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1953-01 Report Number: NACA TN 2880
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On the Stability of the Laminar Mixing Region Between Two Parallel Streams in a Gas
Author(s): Lin, C. C. Corporate Author: Massachusetts Institute of Technology Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1953-01 Report Number: NACA TN 2887
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An Application of the Method of Characteristics to Two-Dimensional Transonic Flows with Detached Shock Waves
Author(s): Harder, Keith C. Corporate Author: Langley Aeronautical Laboratory Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1953-03 Report Number: NACA TN 2910
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An Investigation utilizing and Electrical Analogue of Cyclic De-Icing of a Hollow Steel Propeller with an External Blade Shoe
Author(s): Neel, Carr B. Corporate Author: National Advisory Committee for Aeronautics Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1952-09-30 Report Number: NACA TN 2852
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Impingement of Cloud Droplets on Aerodynamic Bodies as Affected by Compressibility of Air Flow Around the Body
Author(s): Brun, Rinaldo J. Corporate Author: National Advisory Committee for Aeronautics Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1953-03 Report Number: NACA TN 2903
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Investigation of Spontaneous Ignition Temperatures of Organic Compounds with Particular Emphasis on Lubricants
Author(s): Frank, Charles E. Corporate Author: University of Cincinnati Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1952-02 Report Number: NACA TN 2848
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An Analysis of the Factors Affecting the Loss in Lift and Shift in Aerodynamic Center Produced by the Distortion of a Swept Wing Under Aerodynamic Load
Author(s): Mathews, Charles W. Corporate Author: Langley Aeronautical Laboratory Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1953-03 Report Number: NACA TN 2901
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Factors Affecting Laminar Boundary Layer Measurements in a Supersonic Stream
Author(s): Blue, Robert E. Corporate Author: Lewis Flight Propulsion Laboratory Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1953-02 Report Number: NACA TN 2891
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The Planing Characteristics of Two V-Shaped Prismatic Surfaces Having Angles of Dead Rise of 20 and 40
Author(s): Chambliss, Derrill B. Corporate Author: Langley Aeronautical Laboratory Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1953-01 Report Number: NACA TN 2876
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Evaluation of Gust Response Characteristics of Some Existing Aircraft with Wing Bending Flexibility Included
Author(s): Kordes, Eldon E. Corporate Author: Langley Aeronautical Laboratory Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1953-02 Report Number: NACA TN 2897
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Effect of Processing Variables on the Transition Temperature, Strength, and Ductility of High-Purity, Sintered, Wrought Molybdenum Metal
Author(s): Dike, Kenneth D. Corporate Author: Lewis Flight Propulsion Laboratory Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1953-03 Report Number: NACA TN 2915
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Estimated Power Reduction by Water Injection in a Nonreturn Supersonic Wind Tunnel
Author(s): Cooper, Morton Corporate Author: Langley Aeronautical Laboratory Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1953-01 Report Number: NACA TN 2856
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Unsteady Oblique Interaction of a Shock Wave with a Plane Disturbance
Author(s): Moore, Franklin K. Corporate Author: Lewis Flight Propulsion Laboratory Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1953-01 Report Number: NACA TN 2879
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Matrix Methods for Determining the Longitudinal-Stability Derivatives of an Airplane from Transient Flight Data
Author(s): Donegan, James J. Corporate Author: Langley Aeronautical Laboratory Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1953-03 Report Number: NACA TN 2902
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Effect of Horizontal-Tail Span and Vertical Location on the Aerodynamic Characteristics of an Unswept Tail Assembly in Sideslip
Author(s): Riley, Donald R. Corporate Author: Langley Aeronautical Laboratory Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1953-03 Report Number: NACA TN 2907
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Investigation of Gases Evolved During Firing of Vitreous Coatings on Steel
Author(s): Moore, Dwight G. Corporate Author: National Bureau of Standards Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1953-01 Report Number: NACA TN 2865
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Power-Off Flare-Up Tests of a Model Helicopter Rotor in Vertical Autorotation
Author(s): Slaymaker, E. Corporate Author: Princeton University Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1953-01 Report Number: NACA TN 2870
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Average Skin-Friction Drag Coefficients from Tank Tests of a Parabolic Body of Revolution
Author(s): Mottard, Elmo J. Corporate Author: Langley Research Center Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1953-01 Report Number: NACA TN 2854
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Study of Pressure Effects on Vaporization Rate of Drops in Gas Streams
Author(s): Ingebo, Robert D. Corporate Author: Lewis Flight Propulsion Laboratory Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1953-01 Report Number: NACA TN 2850
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Experimental Investigaation of Loss in an Annular Cascade of Turbine Nozzle Blades of Free Vortex Design
Author(s): Allen, Hubert W. Corporate Author: Lewis Flight Propulsion Laboratory Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1953-01 Report Number: NACA TN 2871
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Spiral Motions of Viscous Fluids
Author(s): Hamel, George Corporate Author: National Advisory Committee for Aeronautics Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1953-01 Report Number: NACA TM 1342
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Convection of a Pattern of Vorticity Through a Shock Wave
Author(s): Ribner, H. S. Corporate Author: Lewis Flight Propulsion Laboratory Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1953-01 Report Number: NACA TN 2864
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Study of Secondary-Flow Patterns in an Annular Cascade of Turbine Nozzle Blades with Vortex Design
Author(s): Rohlik, Harold E. Corporate Author: Lewis Flight Propulsion Laboratory Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1953-02 Report Number: NACA TN 2909
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A Study of the Application of Power-Spectral Methods of Generalized Harmonic Analysis to Gust Loads on Airplanes
Author(s): Press, Harry Corporate Author: Langley Aeronautical Laboratory Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1953-01 Report Number: NACA TN 2853
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An Airborne Indicator for Measuring Vertical Velocity of Airplanes at Wheel Contact
Author(s): Dreher, Robert C. Corporate Author: National Advisory Committee for Aeronautics Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1953-02 Report Number: NACA TN 2906
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Icing Protection for a Turbojet Transport Airplane: Heating Requirements, Methods of Protection, and Performance Penalties
Author(s): Gelder, Thomas F. Corporate Author: Lewis Flight Propulsion Laboratory Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1953-01 Report Number: NACA TN 2866
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X-Ray Instrumentation for Density Measurements in a Supersonic Flow Field
Author(s): Dimeff, John Corporate Author: National Advisory Committee for Aeronautics Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1952-02 Report Number: NACA TN 2845
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Theoretical Calculation of the Pressure Distribution, Span Loading, and Rolling Moment Due to Sideslip at Supersonic Speeds for Thin Sweptback Tapered Wings with Supersonic Trailing Edges and Wing Tips Parallel to the Axis of Wing Symmetry
Author(s): Margolis, Kenneth Corporate Author: Langley Aeronautical Laboratory Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1953-02 Report Number: NACA TN 2898
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A Rapid Method for Estimating the Separation Point of a Compressible Laminar Boundary Layer
Author(s): Loftin, Lawrence K. Corporate Author: Langley Aeronautical Laboratory Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1953-02 Report Number: NACA TN 2892
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The Effect Longitudinal Stiffeners Located on One Side of a Plate on the Compressive Buckling Stress of the Plate-Stiffener Combination
Author(s): Seide, Paul Corporate Author: Langley Aeronautical Laboratory Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1953-01 Report Number: NACA TN 2873
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Combined Effects of Damping Screens and Stream Convergence on Turbulence
Author(s): Tucker, Maurice Corporate Author: Lewis Flight Propulsion Laboratory Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1953-01 Report Number: NACA TN 2878
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The Calculation of Pressure on Slender Airplanes in Subsonic and Supersonic Flow
Author(s): Heaslet, Max A. Corporate Author: Ames Aeronautical Laboratory Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1953-03 Report Number: NACA TN 2900
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Behavior in Pure Bending of a Long Monocoque Beam of Circular-Arc Cross Section
Author(s): Fralich, Robert W. Corporate Author: Langley Aeronautical Laboratory Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1953-01 Report Number: NACA TN 2875
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Laminar Natural-Convection Flow and Heat Transfer of Fluids with and without Heat Sources in Channels with Constant Wall Temperatures - and Appendixes A and B
Author(s): Ostrach, Simon Corporate Author: National Advisory Committee for Aeronautics Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1952-02 Report Number: NACA TN 2863
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Calculations of Upwash in the Region Above or Below the Wing-Chord Planes of Swept-Back Wing-Fuselage-Nacelle Combinations
Author(s): Rogallo, Vernon L. Corporate Author: Ames Aeronautical Laboratory Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1953-02 Report Number: NACA TN 2894
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A Low-Speed Experimental Study of the Directional Characteristics of a Sharp-Nosed Fuselage Through a Large Angle-of-Attack Range at Zero Angle of Sideslip
Author(s): Letko, William Corporate Author: Langley Aeronautical Laboratory Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1953-03 Report Number: NACA TN 2911
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