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37 items
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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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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, WilliamCorporate Author(s): Langley Aeronautical Laboratory
Laboratory: National Advisory Committee for Aeronautics
Date of Publication: 1953-03
Report number: NACA TN 2911
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- Serafini, John S. (3)
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