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41 items
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A Rapid Method for Estimating the Separation Point of a Compressible Laminar Boundary Layer
Author(s): Loftin, Lawrence K., Wilson, Homer B.Corporate Author(s): 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): Rogallo, Vernon L., McCloud, John L.Corporate Author(s): 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): Margolis, Kenneth, Sherman, Windsor L., Hannah, Margery E.Corporate Author(s): 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): Heaslet, Max A., Lomax, HarvardCorporate Author(s): 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): Mathews, Charles W., Kurbjun, Max C.Corporate Author(s): 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): Donegan, James J.Corporate Author(s): 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): Brun, Rinaldo J., Serafini, John S., Gallagher, Helen M.Corporate Author(s): 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): Riley, Donald R.Corporate Author(s): 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): Rohlik, Harold E., Allen, Hubert W., Herzig, Howard Z.Corporate Author(s): 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): Harder, Keith C., Klunker, E. B.Corporate Author(s): Langley Aeronautical Laboratory
Laboratory: National Advisory Committee for Aeronautics
Date of Publication: 1953-03
Report number: NACA TN 2910
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- Serafini, John S. (3)
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