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Book Experimental Determination of Airplane Mass and Inertial Characteristics

Download or read book Experimental Determination of Airplane Mass and Inertial Characteristics written by Chester H. Wolowicz and published by . This book was released on 1974 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report reviews and evaluates current practices for experimentally determining airplane center of gravity, moments of inertia, and products of inertia. The techniques discussed are applicable to bodies other than airplanes. In pitching- and rolling-moment-of-inertia investigations with the airplane mounted on and pivoted about knife edges, the non-linear spring moments that occur at large amplitudes of oscillation can be eliminated by using the proper spring configuration. The single-point suspension double-pendulum technique for obtaining yawing moments of inertia, products of inertia, and the inclination of the principal axis provides accurate results from yaw-mode oscillation data, provided that the sway-mode effects are minimized by proper suspension rig design. Rocking-mode effects in the data can be isolated. The conduct of the experiments, as well as the test setup used, is a major factor in obtaining accurate results.

Book The Experimental Determination of the Moments of Inertia of Airplanes by a Simplified Compound pendulum Method

Download or read book The Experimental Determination of the Moments of Inertia of Airplanes by a Simplified Compound pendulum Method written by and published by . This book was released on 1948 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt: A coompound-pendulum method which eliminates the necessity for locating the center of gravity of the airplane by direct measurement is described. The pendulum length is found by measuring the difference between two suspension lengths and solving the equations for the two suspensions simultaneously. Experimental data and a precision analysis are included.

Book NASA Technical Report

    Book Details:
  • Author : United States. National Aeronautics and Space Administration
  • Publisher :
  • Release : 1975
  • ISBN :
  • Pages : 872 pages

Download or read book NASA Technical Report written by United States. National Aeronautics and Space Administration and published by . This book was released on 1975 with total page 872 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book The Experimental Determination of the Moments of Inertia of Airplanes

Download or read book The Experimental Determination of the Moments of Inertia of Airplanes written by Hartley A. Soulé and published by . This book was released on 1933 with total page 15 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Measurement of the Longitudinal Moment of Inertia of a Flexible Airplane

Download or read book Measurement of the Longitudinal Moment of Inertia of a Flexible Airplane written by Henry A. Cole and published by . This book was released on 1956 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt: The application and results of the above method in ground oscillation tests are described. The various corrections to reduce the measured moment of inertia to the reference axis moment of inertia are presented. The results show that measurement of moment of inertia by this method is practicable, provided the knife edges and spring are arranged to minimize excitation of structural modes.

Book A Method for Measuring the Product of Inertia and the Inclination of the Principal Longitudinal Axis of Inertia of an Airplane

Download or read book A Method for Measuring the Product of Inertia and the Inclination of the Principal Longitudinal Axis of Inertia of an Airplane written by Robert W. Boucher and published by . This book was released on 1954 with total page 718 pages. Available in PDF, EPUB and Kindle. Book excerpt: The angle of inclination of the principal axis was found to have probable error of plus or minus 0.17 degrees both from analysis of the error of inertia measurement of the full-scale airplane and from tests with a model having a simple configuration. Analysis showed the probable error of the inertia measurements for the test airplane to be plus or minus1.00, plus or minus 0.49, and plus or minus 0.35 percent of the true moment of inertia about the X, Y, and Z body reference axes, respectively.

Book Experimental Determination of the Moments of Inertia  Product of Inertia  and Inclination of the Principal Axis of Conventional Aircraft by the Spring Oscillation Method

Download or read book Experimental Determination of the Moments of Inertia Product of Inertia and Inclination of the Principal Axis of Conventional Aircraft by the Spring Oscillation Method written by Edward N. Bradfield and published by . This book was released on 1971 with total page 57 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Journal of flight sciences and space research

Download or read book Journal of flight sciences and space research written by and published by . This book was released on 1993 with total page 470 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Experimental Determination of the Three Moments of Inertia and the Product of Inertia in the Plane of Symmetry of the NLR Laboratory Aircraft Siebel 204 D 1

Download or read book Experimental Determination of the Three Moments of Inertia and the Product of Inertia in the Plane of Symmetry of the NLR Laboratory Aircraft Siebel 204 D 1 written by C.H. van der Linden and published by . This book was released on 1963 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Experimental Determination of Stability and Control Aerodynamic Characteristics

Download or read book Experimental Determination of Stability and Control Aerodynamic Characteristics written by R. Fail and published by . This book was released on 1975 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Flight Stability and Automatic Control

Download or read book Flight Stability and Automatic Control written by Robert C. Nelson and published by WCB/McGraw-Hill. This book was released on 1998 with total page 441 pages. Available in PDF, EPUB and Kindle. Book excerpt: The second edition of Flight Stability and Automatic Control presents an organized introduction to the useful and relevant topics necessary for a flight stability and controls course. Not only is this text presented at the appropriate mathematical level, it also features standard terminology and nomenclature, along with expanded coverage of classical control theory, autopilot designs, and modern control theory. Through the use of extensive examples, problems, and historical notes, author Robert Nelson develops a concise and vital text for aircraft flight stability and control or flight dynamics courses.