Flight Investigation of the Effect of Control Centering Springs on the Apparent Spiral Stability of a Personal-owner Airplane PDF Download
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Author: John P. Campbell Publisher: ISBN: Category : Aeronautics Languages : en Pages : 56
Book Description
A flight investigation has been conducted on a typical high-wing personal-owner airplane to determine the effect of control centering springs on apparent spiral stability. The centering springs were used in both the aileron and rudder control systems to provide both a positive centering action and a means of trimming the airplane.
Author: John P. Campbell Publisher: ISBN: Category : Aeronautics Languages : en Pages : 56
Book Description
A flight investigation has been conducted on a typical high-wing personal-owner airplane to determine the effect of control centering springs on apparent spiral stability. The centering springs were used in both the aileron and rudder control systems to provide both a positive centering action and a means of trimming the airplane.
Author: Courtland D. Perkins Publisher: Elsevier ISBN: 1483222330 Category : Technology & Engineering Languages : en Pages : 520
Book Description
Flight Testing, Volume II: Stability and Control focuses on the development of adequate flight test techniques for the appraisal of stability and control characteristics and flying qualities of airplanes. This book discusses the flying quality requirements, longitudinal motions, and flight determination of stick-fixed neutral points. The determination of aerodynamic parameters from steady maneuvering, desirable control characteristics in steady flight, and various forms of lateral control surfaces are also elaborated. This publication likewise covers the measurement of maximum lift coefficient, emergency anti-spin devices, and concept of the altitude-Mach number flight envelope. This volume is recommended for design, development or research engineers, test pilots, and instrumentation personnel interested in airplane stability and control.
Author: Max C. Kurbjun Publisher: ISBN: Category : Noise Languages : en Pages : 742
Book Description
Overall sound-pressure levels and frequency spectra of the noise emitted from a full-scale, 7.2-foot-diameter, 3, 500 rpm, three-blade, supersonic propeller mounted on a turbine-powered airplane have been obtained under static conditions at stations about the propeller at a 100-foot radius.
Author: John P. Campbell
Author: John P. Campbell
Author: United States. National Advisory Committee for Aeronautics
Author: 
Author: United States. National Advisory Committee for Aeronautics
Author: Arthur Earl Bryson
Author: Norman R. Driscoll
Author: Courtland D. Perkins
Author: United States. National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Author: Max C. Kurbjun