Some Structural and Aeroelastic Considerations of High-Speed Flight The Nineteenth Wright Brothers Lecture

[1]  Holt Ashley,et al.  PARAMETRIC STUDIES OF VISCOUS AND NONVISCOUS UNSTEADY FLOWS , 1955 .

[2]  Joseph L. Neuringer,et al.  Aerodynamic Flutter Derivatives for a Flexible Wing with Supersonic and Subsonic Edges , 1955 .

[3]  H. W. Liepmann,et al.  On the Application of Statistical Concepts to the Buffeting Problem , 1952 .

[4]  M. J. Lighthill,et al.  Oscillating Airfoils at High Mach Number , 1953 .

[5]  J. Maxwell,et al.  XV. On the dynamical theory of gases , 1868 .

[6]  Lucien A. Schmit,et al.  THE EFFECTS OF THERMAL RADIATION ON AIRCRAFT STRUCTURES. PART II. THE RESPONSE OF A SIMPLE STRUCTURE TO RADIANT HEATING , 1955 .

[7]  Bo Lundberg.  Fatigue Life of Airplane Structures The Eighteenth Wright Brothers Lecture , 1955 .

[8]  N. J. Hoff,et al.  Approximate analysis of structures in the presence of moderately large creep deformations , 1954 .

[9]  Dean R. Chapman,et al.  Temperature and Velocity Profiles in the Compressible Laminar Boundary Layer with Arbitrary Distribution of Surface Temperature , 1949 .

[10]  A. E. Bryson.  The Effect of Nonuniform Surface Temperature on the Transient Aerodynamic Heating of Thin-Skinned Bodies , 1952 .

[11]  Martin Goland,et al.  An Exact Solution for Two-Dimensional Linear Panel Flutter at Supersonic Speeds , 1954 .

[12]  W. H. Horton.  Laboratory Simulation of Kinetic Heating: A Further Paper from those Presented at the Bristol Conference on Thermal Stress Organized by the Stress Analysis Group of the Institute of Physics , 1954 .

[13]  N. Wiener.  Generalized harmonic analysis , 1930 .