21–27 of 27 hits
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    Tests of six aerofoil sections at various Reynolds numbers in the Compressed Air Tunnel

    Relf, E. F. / Jones, R. / Bell, A. H. | SLUB | 1935
    Contributors: Jones, R. , Bell, A. H.

    An experimental investigation of the characteristics of some plane and cambered 65o delta wings at Mach numbers from 0.7 to 2.0

    Squire, Leonard C. / Jones, J. G. / Stanbrook, A. | SLUB | 1963
    Contributors: Jones, J. G. , Stanbrook, A.

    Tests of six aerofoil sections at various Reynolds numbers in the compressed air tunnel

    Relf, E. F. / Jones, R. / Bell, A. H. | SLUB | 1936
    Contributors: Jones, R. , Bell, A. H.

    Tests on two streamline bodies in the compressed air tunnel

    Jones, R. / Williams, D. H. / Brown, A. F. | SLUB | 1937
    Contributors: Jones, R. , Brown, A. F.

    Approximations to functions and to the solutions of differential equations

    Frazer, R. A. / Jones, William Neville Prichard / Skan, Sylvia W. | SLUB | 1937
    Contributors: Frazer, R. A. , Jones, William Neville Prichard

    The full costs and benefits of transportation : contributions to theory, method and measurement ; with 62 tables

    Greene, David L. / Jones, Donald W. / Delucchi, Mark A. | SLUB | 1997
    Contributors: Jones, Donald W. , Delucchi, Mark A.