Structural Response To Discrete And Continuous Gusts Of An Airplane Having Wing Bending Flexibility And A Correlation Of Calculated And Flight Results
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Structural Response to Discrete and Continuous Gusts of an Airplane Having Wing bending Flexibility and a Correlation of Calculated and Flight Results
Author | : Antonio Ferri,E. R. G. Eckert,John C. Houbolt,Max. A. Heaslet,Merwin Sibulkin,Milton Van Dyke,Murray Tobak,Rose L. Schalla,Walter Castles,United States. National Advisory Committee for Aeronautics,Eldon E. Kordes,Harvard Lomax,Jacob Henri de Leeuw,John N. B. Livingood,Louis M. Nucci,Thomas P. Clark,Glen E. McDonald |
Publsiher | : Unknown |
Total Pages | : 278 |
Release | : 1954 |
Genre | : Aerodynamic load |
ISBN | : OSU:32435025004755 |
Download Structural Response to Discrete and Continuous Gusts of an Airplane Having Wing bending Flexibility and a Correlation of Calculated and Flight Results Book in PDF, Epub and Kindle
Annual Report National Advisory Committee for Aeronautics
Author | : United States. National Advisory Committee for Aeronautics |
Publsiher | : Unknown |
Total Pages | : 135 |
Release | : 1955 |
Genre | : Aeronautics |
ISBN | : STANFORD:36105024166121 |
Download Annual Report National Advisory Committee for Aeronautics Book in PDF, Epub and Kindle
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
NASA Technical Report
Author | : Anonim |
Publsiher | : Unknown |
Total Pages | : 540 |
Release | : 1964 |
Genre | : Aerodynamics |
ISBN | : MINN:31951000846626X |
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Technical Note National Advisory Committee for Aeronautics
Author | : United States. National Advisory Committee for Aeronautics |
Publsiher | : Unknown |
Total Pages | : 348 |
Release | : 1958 |
Genre | : Aeronautics |
ISBN | : OSU:32435026187393 |
Download Technical Note National Advisory Committee for Aeronautics Book in PDF, Epub and Kindle
Relationship of Metal Surfaces to Heat aging Properties of Adhesive Bonds
Author | : J. M. Black,R. F. Blomquist |
Publsiher | : Unknown |
Total Pages | : 696 |
Release | : 1958 |
Genre | : Adhesives |
ISBN | : STANFORD:36105024832490 |
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A study was made to determine the probable causes of deterioration of each of several adhesives in bonds to stainless steel at temperatures from 400 to 550 degrees F. Prellminary studies of aluminum surfaces on which ions of metals used in staLnless steel were introduced showed that iron was probably catalyzing a thermal deterioration of the adhesive. The resistance of FPL-878 adhesive to thermal deterioration at 550 degrees F on steel was improved signiffcantly by treating the steel surface to be bonded with either zinc or cerium naphthenate and firing at 1,200 degrees F. The addition of manganese dioxide to the adhesive also increased its resistance to thermal deterioration. A study of the thermal-aging properties of five different chemical types of adhesives on stainless steel and alumina revealed that a phenol-nitrile rubber adhesive was superior to a phenol-epoxy adhesive on steel, but this order was reversed on alumina. These and other observations indicated probable specific relationships among the chemical structure of the adhesive, the metal adherend, and the resultant thermal stability of bonds after aging at high temperatures.
Subsonic Flight Investigation of Methods to Improve the Damping of Lateral Oscillations by Means of a Viscous Damper in the Rudder System in Conjuction with Adjusted Hinge moment Parameters
Author | : Harold L. Crane |
Publsiher | : Unknown |
Total Pages | : 654 |
Release | : 1958 |
Genre | : Airplanes |
ISBN | : STANFORD:36105024832391 |
Download Subsonic Flight Investigation of Methods to Improve the Damping of Lateral Oscillations by Means of a Viscous Damper in the Rudder System in Conjuction with Adjusted Hinge moment Parameters Book in PDF, Epub and Kindle
A flight investigation at subsonic speeds of a method to improve the damping of lateral oscillations by means of a viscous damping cylinder used in the rudder system in conjunction with adjusted hinge-moment parameters has been conducted. The damping device has been applied to a modern fighter-type jet-powered airplane. The rudder was made to float with the relative wind by the addition of trailing-edge strips. In order to amplify the floating tendency (by reducing the restoring moment), a highly geared balancing tab was incorporated. Lag of the motion of the free rudder with respect to the yawing of the airplane was introduced by means of a small viscous damping cylinder linked to the rudder.