Fatigue Test and Analysis of the F-100 Landing Gear. Volume I, (2002)
Andrews,W., Carter,A. L., Harsfall,W., Troke,R. W.
A static strength analysis is performed using revised and up-dated ground loads for the new F-100 landing gear, as redesigned under the direction of OOAMA, Hill Air Force Base, Ogden, Utah. No zero...
Fatigue Test and Analysis of the F-100 Landing Gear. Volume II, (2002)
Andrews,W., Carter,A. L., Horsfall,W., Troke,R. W.
This section describes the experimental stress analysis phase of the landing gear fatigue investigation. The objectives of the experimental phase were: determine the peak stress points and associated...
Fatigue Test and Analysis of the F-100 Landing Gear. Volume III, (2002)
Andrews,W., Carter,A. L., Horsfall,W., Troke,R. W.
The F-100 Aircraft Structural Integrity Program was designed to fatigue test the basic wing, fuselage and empennage structure of the air vehicle. In conjunction with these tests, actual nose and main...
Fatigue Test and Analysis of the F-100 Landing Gear. Appendices A and B, (2002)
Andrews,W., Carter,A. L., Horsfall,W., Troke,R. W.
See also Volume 3 dated 15 Aug 69, AD-A008 463, and Appendix C dated 15 Aug 69, AD-A008 465.
Fatigue Test and Analysis of the F-100 Landing Gear. Appendix C, (2002)
Andrews,W., Carter,A. L., Horsfall,W., Troke,R. W.
See also Appendices A and B dated 15 Aug 69, AD-A008 464.
Fatigue Test and Analysis of the F-100 Landing Gear. Appendix D, (2002)
Andrews,W., Carter,A. L., Horsfall,W., Troke,R. W.
See also Appendix C dated 15 Aug 75, AD-A008 465.
Ko, W.L., Carter, A.L., Totton, W.W., Ficke, J.M.
Stress intensity levels at various parts of the NASA B-52 carrier aircraft pylon were examined for the case when the pylon store was the space shuttle solid rocket booster drop test vehicle. Eight...