Advisory Report, Issue 1; Issue 8; Issues 10-13The Organization, 1965 - Aerodynamics |
Contents
SUMMARY REPORT | 2 |
CONCLUSIONS AND RECOMMENDATIONS | 12 |
UNITED KINGDOM | 17 |
35 other sections not shown
Other editions - View all
Common terms and phrases
accuracy aerodynamic Aeroelastic Aeronautical Aerospace AGARD AIAA aircraft aluminum alloy analysis application aspect ratio axial bilayer blade boundary layer buckling calculated Composite Materials compression configuration constant crack length crack strength critical cruise CSA method curve cylindrical shells data from Reference edge effect efficiency elastic electrical resistivity engineer Equation experimental factor fatigue cracks filament filamentary composites flat panels flight flutter boundary fracture Fracture Mechanics frequency GALCIT heat helicopter high temperatures isotropic laminate loading longitudinal Mach number measured metals mode multiweb NACA NASA notch strength obtained orthotropic Panel Flutter parameter phonons plot pop-in prediction pressure problem radial range Report Research residual strength rotor Royal Aeronautical Society sandwich Section shear shown in Figure simply-supported specimens speed Stability stiffened structural studies Supersonic Supersonic Flow tensile strength test data theoretical thermal conductivity thermocouples thermophysical properties thickness two-dimensional values vibration VTOL weight width wing