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Book Investigation of the Air compression Process During Drop Tests of an Oleo pneumatic Landing Gear

Download or read book Investigation of the Air compression Process During Drop Tests of an Oleo pneumatic Landing Gear written by James H. Walls and published by . This book was released on 1951 with total page 786 pages. Available in PDF, EPUB and Kindle. Book excerpt: A brief study has been made to evaluate the importance of the type of air-compression process on the loads produced on an oleo-pneumatic landing gear during impact and to determine the type of air compression process actually obtained during drop tests. A simplified analysis to determine the effect which different air-compression processes might have indicates that the value of the air-compression exponent should have relatively little effect on the landing-gear loads throughout most of the impact. The analysis of experimental data obtained in these tests shows that the polytropic exponent ranged from 1.01 to 1.10 for the condtions tested. The general trend of the data appears relatively independent of vertical contact velocity.

Book Technical Note   National Advisory Committee for Aeronautics

Download or read book Technical Note National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1955 with total page 924 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Technical Note

Download or read book Technical Note written by and published by . This book was released on 1951 with total page 656 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book A Study of Analytic Modeling Techniques for Landing Gear Dynamics

Download or read book A Study of Analytic Modeling Techniques for Landing Gear Dynamics written by and published by . This book was released on 1982 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt: The ability to accurately predict the dynamic response of an aircraft while it is operating in the taxi mode depends, in part on the correct modeling of the dynamic characteristics of the landing gear system. Traditionally, landing gear have been designed to absorb landing impact ('shock absorber') and their characteristics during periodic, oscillatory response ('spring') have been considered as secondary. With the increased emphasis on the rough or damaged field taxi operation, there is a requirement to determine the best methods for modeling the gear system. This report documents a brief review of the state of the art of gear modeling. A study was then conducted to evaluate important model parameters, using a simple cantilevered gear computer simulation. Also included is the development of a technique for the experimental determination of important gear system parameters. (Author).

Book Bibliography of Technical Reports

Download or read book Bibliography of Technical Reports written by and published by . This book was released on 1952 with total page 500 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Annual Report   National Advisory Committee for Aeronautics

Download or read book Annual Report National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1955 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.

Book A Comparison of the Experimental Subsonic Pressure Distributions about Several Bodies of Revolution with Pressure Distributions Computed by Means of the Linearized Theory

Download or read book A Comparison of the Experimental Subsonic Pressure Distributions about Several Bodies of Revolution with Pressure Distributions Computed by Means of the Linearized Theory written by Albert J. Evans and published by . This book was released on 1953 with total page 326 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Report   National Advisory Committee for Aeronautics

Download or read book Report National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1952 with total page 1208 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Research Abstracts

    Book Details:
  • Author : United States. National Advisory Committee for Aeronautics
  • Publisher :
  • Release : 1951
  • ISBN :
  • Pages : 568 pages

Download or read book Research Abstracts written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1951 with total page 568 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book A Compilation of Research Reports of Physical Research Division  Dynamic Loads Division  Loads Division  1921   1973

Download or read book A Compilation of Research Reports of Physical Research Division Dynamic Loads Division Loads Division 1921 1973 written by Gloria R. Champine and published by . This book was released on 1977 with total page 134 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Annual Report

    Book Details:
  • Author : United States. National Advisory Committee for Aeronautics
  • Publisher :
  • Release : 1953
  • ISBN :
  • Pages : 534 pages

Download or read book Annual Report written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1953 with total page 534 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Report

    Book Details:
  • Author :
  • Publisher :
  • Release : 1956
  • ISBN :
  • Pages : 1044 pages

Download or read book Report written by and published by . This book was released on 1956 with total page 1044 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Noise Survey of a 10 foot Four blade Turbine driven Propeller Under Static Condtions

Download or read book Noise Survey of a 10 foot Four blade Turbine driven Propeller Under Static Condtions written by Max C. Kurbjun and published by . This book was released on 1955 with total page 686 pages. Available in PDF, EPUB and Kindle. Book excerpt: Theoretical calculations of the sound-pressure levels by the method of NACA TN 2968 predict accurately, for the 10-foot propeller investigated, the location of and the maximum levels to be expected for the overall noise and the first two propeller harmonics. The calculations do not predict accurately the location of the maximum sound-pressure levels ad the maximum calculated levels are 10 and 13 decibels lower than the msximm messured levels for the third and fourth harmonics, respectively.

Book List of Technical Notes  1947 1953

Download or read book List of Technical Notes 1947 1953 written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1954 with total page 162 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Wind tunnel and Flight Investigations of the Use of Leading edge Area Suction for the Purpose of Increasing the Maximum Lift Coefficient of a 35   swept wing Airplane

Download or read book Wind tunnel and Flight Investigations of the Use of Leading edge Area Suction for the Purpose of Increasing the Maximum Lift Coefficient of a 35 swept wing Airplane written by Curt A. Holzhauer and published by . This book was released on 1956 with total page 284 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Applied Mechanics Reviews

Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1952 with total page 626 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Report

    Book Details:
  • Author : United States. National Advisory Committee for Aeronautics
  • Publisher :
  • Release : 1956
  • ISBN :
  • Pages : 36 pages

Download or read book Report written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1956 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: