Aeronautical Research at the University of Southampton

F. W. Lanchester obtained his first technical education at the Hartley Institute in Southampton, later to become the University of Southampton, during the years 1886–89. His autobiography describes in vivid terms the primitive nature of the workshop and apparatus available. He would indeed be shocked at the wealth of modern equipment now encountered in engineering departments of a University. At the same time, no one can possibly say that this lack of equipment influenced his pioneer spirit or his extraordinary clarity of thought, not only in the fields of aeronautical and automobile engineering, but also in subjects as diverse as the musical scale, poetry and even relativity.

[1]  C. L. Morfey,et al.  Rotating pressure patterns in ducts: Their generation and transmission , 1964 .

[2]  M. R. C. McDowell,et al.  Atomic Collision Processes , 1965 .

[3]  E. J. Richards Research on Aerodynamic Noise From Jets and Associated Problems , 1953, The Journal of the Royal Aeronautical Society.

[4]  Michael Fisher,et al.  The characteristics of the turbulence in the mixing region of a round jet , 1963, Journal of Fluid Mechanics.

[5]  A. J. Pretlove Bond stresses in a randomly vibrating sandwich plate: Multi-modal theory , 1965 .

[6]  Robert Hugh Macmillan,et al.  Progress in control engineering , 1962 .

[7]  P. E. Doak,et al.  Analysis of internally generated sound in continuous materials: (I) inhomogeneous acoustic wave equations , 1965 .

[8]  E. J. Richards,et al.  A New Concept in the Design of Jet Engine Mufflers and Test Cells , 1957, Journal of the Royal Aeronautical Society.

[9]  Jeffrey P. Jones,et al.  The Use of an Analogue Computer to Calculate Rotor Blade Motion , 1964 .

[10]  A. J. Pretlove Free vibrations of a rectangular panel backed by a closed rectangular cavity by a closed rectangular cavity , 1965 .

[11]  P. E. Doak The reflexion of a spherical acoustic pulse by an absorbent infinite plane and related problems , 1952, Proceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences.

[12]  D. J. Mead The practical problems of assessing damping treatments , 1964 .

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

[15]  J.P.A. Lochner,et al.  The influence of reflections on auditorium acoustics , 1964 .

[16]  M. V. Lowson The separated flow on slender wings in unsteady motion , 1963 .

[17]  R. C. Potter Measurements of the turbulence in interfering mixing regions from jets , 1963 .

[18]  Denys J Mead,et al.  INTERFACE DAMPING AT RIVETED JOINTS. PART II. DAMPING AND FATIGUEMEASUREMENTS. , 1965 .

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[22]  D. J. Mead The Effect of a Damping Compound on Jet‐Efflux Excited Vibrations , 1960 .

[23]  B. L. Clarkson,et al.  The Response of a Typical Aircraft Structure to Jet Noise , 1962, The Journal of the Royal Aeronautical Society.

[24]  Alan Powell,et al.  A Survey of Experiments on Jet Noise , 1954 .

[25]  D. J. Mead Bond stresses in a randomly vibrating sandwich plate: Single mode theory , 1964 .

[26]  T. Tanner A Survey of Yacht Research at Southampton University , 1962 .

[27]  B. L. Clarkson The Design of Structures to Resist Jet Noise Fatigue , 1962, The Journal of the Royal Aeronautical Society.

[28]  P. C. Parks,et al.  A STABILITY CRITERION FOR A PANEL FLUTTER PROBLEM VIA THE SECOND METHOD OF LIAPUNOV , 1965 .

[29]  E. E. Zepler,et al.  The loudness of sonic booms and other impulsive sounds , 1966 .

[30]  G. E. Merritt,et al.  Hypersonic laminar flow over cavities and steps , 1964 .

[31]  R. E. Franklin Space-Correlations in the Fluctuating Pressure Field Near to a Jet Engine , 1961, The Journal of the Royal Aeronautical Society.

[32]  Alan Powell,et al.  On the Fatigue Failure of Structures due to Vibrations Excited by Random Pressure Fields , 1958 .

[33]  I. J. Sharland Sources of noise in axial flow fans , 1964 .

[34]  P. J. Musgrove The influence of the boundary layer on shock tube running times , 1964 .

[35]  M. Petyt THE APPLICATION OF FINITE ELEMENT TECHNIQUES TO PLATE AND SHELL PROBLEMS. , 1965 .

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[37]  E. J. Richards,et al.  SOME PRACTICAL APPLICATIONS OF BOUNDARY LAYER PRESSURE FLUCTUATION WORK , 1963 .

[38]  D. J. Mead Criteria for Comparing the Effectiveness of Damping Treatments , 1961 .

[39]  R. E. Franklin,et al.  The Vibrations of a Thin-Walled Stiffened Cylinder in an Acoustic Field , 1959 .

[40]  J. P. Appleton,et al.  The conservation equations for a non-equilibrium plasma , 1964, Journal of Fluid Mechanics.

[41]  P. Davies,et al.  Heat transfer from electrically heated cylinders , 1964, Proceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences.

[42]  R. E. Franklin Noise Measurements on Cold Jets using Convergent-Divergent Nozzles , 1957 .

[43]  E. R. Lindgren,et al.  THE TRANSITION PROCESS AND OTHER PHENOMENA IN VISCOUS FLOW , 1957 .

[44]  J. E. F. Williams Noise from Convected Turbulence , 1961 .

[45]  D. R. Blackman,et al.  Wall pressure fluctuations in the laminar turbulent transition region of a boundary layer , 1964 .

[46]  M. Judd The Effect of a Root Gap on the Aerodynamic Forces of a Slender Delta Wing in Oscillatory Pitching Motion , 1963 .

[47]  J. P. Appleton Structure of a Prandtl‐Meyer Expansion in an Ideal Dissociating Gas , 1963 .