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The Aeronautical Research Scene -Goals, Methods and Accomplishments

Published online by Cambridge University Press:  28 July 2016

Hugh L. Dryden
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Extract

Prizes were presented and The Thirty-seventh Wilbur Wright Lecture was delivered before The Royal Aeronautical Society at the Royal Institution, 21 Albemarle Street, London, W.l, on Thursday 28th April 1949. Dr. H. Roxbee Cox, B.Sc., D.I.C., F.I.Ae.S., F.R.Ae.S., President, presided at the meeting.

Type
37th Wilbur Wright Lecture
Information
The Aeronautical Journal , Volume 53 , Issue 463 , July 1949 , pp. 623 - 666
Copyright
Copyright © Royal Aeronautical Society 1949

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References

1. von Karman, TH. Supersonic Aerodynamics —Principles and Applications. Jour. Aero. Sci., vol. 14, pp. 373–402, 1947.Google Scholar
2. Lighthill, M. T. Methods for Predicting Phenomena in the High-Speed Flow of Gases. Jour. Aero. Sci., vol. 16, pp. 69–83, 1949.Google Scholar
3. Cope, W. F., and Hartree, D. R. The Laminar Boundary Layer in Compressible Flow. Phil. Trans. Roy. Soc. (London), vol. 241, pp. 1–69, 1948.Google Scholar
4. Tsien, H. S., and Finsten, M. Interaction between Parallel Streams of Subsonic and Supersonic Velocities. To be published in Jour. Aero. Sci., 1949.Google Scholar
5. Kane, E. D., and Folsom, R. G. Problems and Progress in Low-Pressure Research. Jour. Aero. Sci., vol. 16, pp. 46–54, 1949.Google Scholar
6. Tsien, H. S. Superaerodynamics, Mechanics of Rarefied Gases. Jour. Aero. Sci., vol. 13, pp. 653–664, 1946.CrossRefGoogle Scholar
7. Tsien, H. S. Wind-Tunnel Testing Problems in Superaerodynamics. Jour. Aero. Sci., vol. 15, pp. 573–580, 1948.Google Scholar
8. Linnell, R. D. Two-Dimensional Airfoils in Hypersonic Flows. Jour. Aero. Sci., vol. 16, pp. 22–30, 1949.Google Scholar
9. Williams, T. W., and Benson, J. M. Preliminary Investigation of the Use of Afterglow for Visualising Low-Density Compressible Flows. To be published as N.A.C.A. Tech. Note.Google Scholar
10. Prager, W. Recent Developments in the Mathematical Theory of Plasticity. Paper presented at Seventh International Congress for Applied Mechanics, September 1948. See also The Stress-Strain Laws of Mathematical Theory of Plasticity—A Survey of Recent Progress. Jour. Appl. Mech., vol. 15, no. 3, pp. 226–233, 1948.CrossRefGoogle Scholar
11. Drucker, D. C. Relation of Experiments to Mathematical Theories of Plasticity. A.S.M.E. paper no. 49-A.P.M.-5, to be published in jour. Appl. Mech., 1949.Google Scholar
12. Batdorf, S. B. Theories of Plastic Buckling. To be published in Jour. Aero. Sci., 1949.Google Scholar
13. Batdorf, S. B., and Budiansky, B. A New Mathematical Theory of Plasticity Based on the Concept of Slip. To be published as N.A.C.A. Tech. Note.Google Scholar
14. Schubauer, G. B., and Skramstad, H. K. Laminar Boundary-Layer Oscillations and Transition on a Flat Plate. N.A.C.A. Wartime Report W-8; also Journal of Research of the National Bureau of Standards, vol. 38, pp. 251–292, 1947; also N.A.C.A. Tech. Report.Google Scholar
15. Dryden, H. L. Some Recent Contributions to the Study of Transition and Turbulent Boundary Layers. N.A.C.A. Tech. Note 1188, 1947.Google Scholar
16. Chiarulli, P., and Freeman, J. C. Stability of the Boundary Layer. U.S. Air Materiel Command Tech. Report F.-T.R.-l1971A.Google Scholar
17. Dryden, H. L. Recent Advances in the Mechanics of Boundary Layer Flow. Advances in Applied Mechanics, vol. 1, pp. 1–40, 1948.Google Scholar
18. Lees, L., and Lin, C. C. Investigation of the Stability of the Laminar Boundary Layer in a Compressible Fluid. N.A.C.A. Tech. Note 1115, 1946.Google Scholar
19. Lees, L. The Stability of the Laminar Boundary Layer in a Compressible Fluid. N.A.C.A. Technical Note 1360, 1947.Google Scholar
20. Heisenbero, W. Zur statistischen Theorie der Turbulenz. Zeitschrift für Physik, vol. 124, pp. 628–657, 1947.Google Scholar
21. Von Karman, TH. Progress in the Statistical Theory of Turbulence. Proc. Nat. Acad. Sci., vol. 34, pp. 530–539, 1948.Google Scholar
22. Gooderum, P. B., Wood, G. P., and Brevoort, M. T. Investigation with an Interferometer of the Turbulent Mixing of a Free Supersonic Jet. To be published as N.A.C.A. Tech. Note.Google Scholar
23. Scurlock, A. C. Flame Stabilisation and Propagation in High-Velocity Gas Streams. Meteor. Report no. 19, Massachusetts Institute of Technology, Guided Missiles Program, Cambridge 39, Massachusetts, May 1948.Google Scholar
24. Perkins, E. W. Experimental Investigation of the Effects of Support Interference on the Drag of Bodies of Revolution at a Mach Number of 1.5. To be published as N.A.C.A. Tech. Note.Google Scholar
25. Kemp, R. H., Morgan, W. C., and Manson, S. S. The Application of High-Temperature Strain Gages to the Measurement of Vibratory Stresses in Gas-Turbine Buckets. N.A.C.A. Tech. Note 1174, 1947.Google Scholar
26. Baals, D. B., Smith, N. F., and Wright, J. B. The Development and Application of High-Critical-Speed Nose Inlets. N.A.C.A. Wartime Report L.-729 (originally A.C.R. L5F30A, 1945).Google Scholar
27. Smith, N. F., and Baals, D. B. Wind-Tunnel Investigation of a High-Critical-Speed Fuselage Scoop Including the Effects of Boundary Layer. N.A.C.A. Wartime Report L.-733 (originally A.C.R. L5B01A, 1945).Google Scholar
28. Schey, O. W. The Advantages of High Inlet Temperature for Gas Turbines and Effectiveness of Various Methods of Cooling the Blades. A.S.M.E. Paper No. 48-A.-105, 1948. Annual Meeting, American Society of Mechanical Engineers.Google Scholar