The Second Lanchester Memorial Lecture

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[2]  H. Glauert.  The force and moment on an oscillating aerofoil , 1930 .

[3]  J. C. Floyd.  The Fourteenth British Commonwealth Lecture: The Canadian Approach to All-Weather Interceptor Development , 1958 .

[4]  F. Smith,et al.  Design of a Simple Electronic Flutter Simulator , 1953 .

[5]  R. A. Frazer.  The Flutter of Aeroplane Wings , 1929, Journal of the Royal Aeronautical Society.

[6]  A. S. Taylor.  The Present Status of Aircraft Stability Problems in the Aeroelastic Domain , 1959 .

[7]  A. R. Collar,et al.  Aeroelastic Problems at High Speed , 1947, The Journal of the Royal Aeronautical Society.

[8]  A. R. Collar,et al.  The Expanding Domain of Aeroelasticity , 1946, The Journal of the Royal Aeronautical Society.

[9]  Charles C. Kennedy,et al.  Use of Vectors in Vibration Measurement and Analysis , 1947 .

[10]  J. H. Argyris,et al.  Some Effects of Kinetic Heating on the Stiffness of Thin Wings‐II , 1957 .

[11]  W. G. BICKLEY.  Mechanical Admittances and their Applications to Oscillation Problems , 1948, Nature.

[13]  E. J. Richards.  On the Noise from Supersonic Jets , 1957, The Journal of the Royal Aeronautical Society.

[14]  Herbert Wagner.  Über die Entstehung des dynamischen Auftriebes von Tragflügeln , 1925 .

[15]  W. J. Duncan.  The Fundamentals of Flutter , 1945 .

[16]  A. G. Pugsley.  Control Surface and Wing Stability Problems , 1937 .

[17]  H. Roxbee Cox.  Problems involving the stiffness of aeroplane wings , 1934 .

[18]  Frazer.  Elementary Matrices: Frontmatter , 1938 .