THEORETICAL STUDIES OF THE EFFECTS OF ASPECT RATIO ON FLUTTER Open PDF Document Details Document Type Technical Report Publication Date Jun 01, 1954 Accession Number AD0050212 Entities People M. A. Dengler Martin Goland Y. L. Luke Organizations MRIGlobal Tags Communities of Interest Air Platforms Human Systems DTIC Thesaurus Topics Accuracy Air Force Aircrafts Airfoils Aspect Ratio Coefficients Construction Equations Intensity Leading Edges Pressure Distribution Schematic Diagrams Steady State Swept Wings Trailing Edges Two Dimensional Wing Tips