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Report Availability
450 reports
Analytical Investigation of Icing Limit for Diamond-Shaped Airfoil in Transonic and Supersonic Flow
Author(s): Edmund E. Callaghan; John S. Serafini 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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Study of Pressure Effects on Vaporization Rate of Drops in Gas Streams
Author(s): Robert D. Ingebo 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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A Study of the Application of Power-Spectral Methods of Generalized Harmonic Analysis to Gust Loads on Airplanes
Author(s): Harry Press; Bernard Mazelsky 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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Average Skin-Friction Drag Coefficients from Tank Tests of a Parabolic Body of Revolution
Author(s): Elmo J. Mottard; J. Dan Loposer 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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Icing Protection for a Turbojet Transport Airplane: Heating Requirements, Methods of Protection, and Performance Penalties
Author(s): Thomas F. Gelder; James P. Lewis; Stanley L. Koutz 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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Estimated Power Reduction by Water Injection in a Nonreturn Supersonic Wind Tunnel
Author(s): Morton Cooper; John R. Sevier 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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Convection of a Pattern of Vorticity Through a Shock Wave
Author(s): H. S. Ribner 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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Power-Off Flare-Up Tests of a Model Helicopter Rotor in Vertical Autorotation
Author(s): E. Slaymaker; Robin B. Gray Corporate Author: Princeton University Laboratory: National Advisory Committee for Aeronautics Date of Publication: 1953-01 Report Number: NACA TN 2870
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A Digital Automatic Multiple Pressure Recorder
Author(s): Bert A. Coss; D. R. Daykin; Leonard Jaffe; Elmer M. Sharp 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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Investigation of Gases Evolved During Firing of Vitreous Coatings on Steel
Author(s): Dwight G. Moore; Mary A. Mason 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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Experimental Investigaation of Loss in an Annular Cascade of Turbine Nozzle Blades of Free Vortex Design
Author(s): Hubert W. Allen; Milton G. Kofskey; Richard E. Chamness 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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Combined Effects of Damping Screens and Stream Convergence on Turbulence
Author(s): Maurice Tucker 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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Unsteady Oblique Interaction of a Shock Wave with a Plane Disturbance
Author(s): Franklin K. Moore 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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The Effect of Initial Curvature on the Strength of an Inelastic Column
Author(s): Eldon. E. Mathauser; William Brooks; Thomas W. Wilder Corporate Author: Langley Aeronautical Laboratory Laboratory: Langley Aeronautical Laboratory Date of Publication: 1953-01 Report Number: NACA TN 2872
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On Traveling Waves in Beams
Author(s): Robert W. Leonard; Bernard Budiansky Corporate Author: Langley Aeronautical Laboratory Laboratory: Langley Aeronautical Laboratory Date of Publication: 1953-01 Report Number: NACA TN 2874
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On the Use of a Damped Sine-wave Elevator Motion for Computing the Design Maneuvering Horizontal-tail Load
Author(s): Melvin Sadoff Corporate Author: Ames Aeronautical Laboratory Laboratory: Ames Aeronautical Laboratory Date of Publication: 1953-01 Report Number: NACA TN 2877
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Theoretical Investigation of the Longitudinal Response Characteristics of a Swept-Wing Fighter Airplane Having a Pitch-Attitude Control System
Author(s): Fred H. Stokes; J. T. Matthews Corporate Author: Langley Aeronautical Laboratory Laboratory: Langley Aeronautical Laboratory Date of Publication: 1953-01 Report Number: NACA TN 2882
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Reflection of Weak Shock Wave from a Boundary Layer Along a Flat Plate. II. Interaction of Oblique Shock Wave with a Laminar Boundary Layer Analyzed by Differential-Equation Method
Author(s): Yung-Huai Kuo Corporate Author: Cornell University Date of Publication: 1953-01 Report Number: NACA TN 2869
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Bearing Strengths of Some 75S-T6 and 14S-T6 Aluminum-Alloy Hand Forgings
Author(s): E. M. Finley Corporate Author: Aluminum Company of America Date of Publication: 1953-01 Report Number: NACA TN 2883
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Calculation and Measurement of Normal Modes of Vibration of an Aluminum-Alloy Box Beam with and without Large Discontinuities
Author(s): Frank C. Smith; Darnley M. Howard Corporate Author: National Bureau of Standards Date of Publication: 1953-01 Report Number: NACA TN 2884
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Cooling of clothed subjects immersed in cold water
Author(s): John F. Hall; Johannes W. Polte Corporate Author: Aero Medical Laboratory Laboratory: Aero Medical Laboratory Date of Publication: 1953-04 Report Number: WADC TR 53-323
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Effect of Flashes of Light Through the Closed Eyelid. Part 2, Use of Dark Grease on the Closed Eyelids as a Means of Preserving Dark Adaptation During a Flash of Light
Author(s): Glenn A. Fry; Norman Ihrig Corporate Author: Ohio State University Research Foundation Laboratory: Aero Medical Laboratory Date of Publication: 1953-02 Report Number: WADC TR 53-159 Part 2
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Factors Affecting Rate of Apparent Change in a Dynamic Ambiguous Figure as a Function of Observation Time
Author(s): Kenneth T. Brown Corporate Author: Aero Medical Laboratory Laboratory: Aero Medical Laboratory Date of Publication: 1953-12 Report Number: WADC TR 53-482
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Human Engineering Design Schedule for Training Equipment
Author(s): Robert B. Miller Corporate Author: American Institute for Research Laboratory: Aero Medical Laboratory Date of Publication: 1953-06 Report Number: WADC TR 53-138
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On the Stability of the Laminar Mixing Region Between Two Parallel Streams in a Gas
Author(s): C. C. Lin 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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Calculation of the Shape of a Two-Dimensional Supersonic Nozzle in Closed Form
Author(s): Dante Cunsolo Date of Publication: 1953-01 Report Number: NACA TM 1358
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Effects of Hypothermia on Brain Activity
Author(s): Werner K. Noell; Stanley A. Briller Corporate Author: Department of Neuropsychiatry Laboratory: School of Aviation Medicine Date of Publication: 1953-01
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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): Alfred Ritter; Yung-Huai Kuo 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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The Effect Longitudinal Stiffeners Located on One Side of a Plate on the Compressive Buckling Stress of the Plate-Stiffener Combination
Author(s): Paul Seide 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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Behavior in Pure Bending of a Long Monocoque Beam of Circular-Arc Cross Section
Author(s): Robert W. Fralich; J. Mayers; Eric Reissner 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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The Planing Characteristics of Two V-Shaped Prismatic Surfaces Having Angles of Dead Rise of 20 and 40
Author(s): Derrill B. Chambliss; George M. Boyd 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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Solid-State and Molecular Theory Group
Corporate Author: Massachusetts institute of Technology Date of Publication: 1953-01-15
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Altitude Effects on Intra-Abdominal Lesions. A. The Effects of Altitude on Induced E. Coli Periontitis in Mice
Author(s): William H. Harridge; Warren H. Cole Corporate Author: University of Illinois College of Medicine Date of Publication: 1953-01
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Psychophysiological Effects of Cold I. The Role of Skin-Temperature and Sensory Sensitivity in Manual Performance Decrement
Author(s): Robert A. McCleary Corporate Author: School of Aviation Medicine Laboratory: School of Aviation Medicine Date of Publication: 1953-01
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Physiological Effects of Mechanical Vibration
Author(s): Victor Guillemin; Pablo Wechsberg Corporate Author: University of Illinois Laboratory: School of Aviation Medicine Date of Publication: 1953-01
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Factors Affecting Laminar Boundary Layer Measurements in a Supersonic Stream
Author(s): Robert E. Blue; George M. Low 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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A Rapid Method for Estimating the Separation Point of a Compressible Laminar Boundary Layer
Author(s): Lawrence K. Loftin; Homer B. Wilson 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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Calculations of Upwash in the Region Above or Below the Wing-Chord Planes of Swept-Back Wing-Fuselage-Nacelle Combinations
Author(s): Vernon L. Rogallo; John L. McCloud 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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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): Kenneth Margolis; Windsor L. Sherman; Margery E. Hannah 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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The Calculation of Pressure on Slender Airplanes in Subsonic and Supersonic Flow
Author(s): Max A. Heaslet; Harvard Lomax 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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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): Charles W. Mathews; Max C. Kurbjun 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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Matrix Methods for Determining the Longitudinal-Stability Derivatives of an Airplane from Transient Flight Data
Author(s): James J. Donegan 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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Impingement of Cloud Droplets on Aerodynamic Bodies as Affected by Compressibility of Air Flow Around the Body
Author(s): Rinaldo J. Brun; John S. Serafini; Helen M. Gallagher 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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Effect of Horizontal-Tail Span and Vertical Location on the Aerodynamic Characteristics of an Unswept Tail Assembly in Sideslip
Author(s): Donald R. Riley 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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Study of Secondary-Flow Patterns in an Annular Cascade of Turbine Nozzle Blades with Vortex Design
Author(s): Harold E. Rohlik; Hubert W. Allen; Howard Z. Herzig 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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An Application of the Method of Characteristics to Two-Dimensional Transonic Flows with Detached Shock Waves
Author(s): Keith C. Harder; E. B. Klunker 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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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): William Letko 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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A Method for Rapid Determination of the Icing Limit of a Body in Terms of the Stream Conditions
Author(s): Edmund E. Callaghan; John S. Serafini 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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Effect of Processing Variables on the Transition Temperature, Strength, and Ductility of High-Purity, Sintered, Wrought Molybdenum Metal
Author(s): Kenneth D. Dike; Roger A. Long 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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N. P. F. Analysis
Author(s): James H. McNeal Corporate Author: University of Delaware Date of Publication: 1953-02
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