21–40 von 2,078 Ergebnissen
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    The development of a flight path recorder suitable for performance testing

    Alston, R. P. / Jones, D. A. / Jones, E. T. | SLUB | 1932
    Beteiligte: Jones, D. A. , Jones, E. T.

    Airflow about stalled and spinning aeroplanes shown by cinematographic records of the movements of wool tufts

    Jones, Bennett Melvill / Haslam, J. A. G. | SLUB | 1933
    Beteiligte: Jones, Bennett Melvill , Haslam, J. A. G.

    Servo Shoe Brake Calculations

    An Analytical Basis for the Study of the Problem of Brakes with any Number of Shoes
    Roxbee Cox, H. / Rowlett Jones, A. | Emerald Group Publishing | 1934

    Tests on aerofoil flaps in the compressed air tunnel

    Jones, R. / Bell, A. H. / Smyth, E. | TIBKAT | 1935

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

    Relf, E. F. / Jones, R. / Bell, A. H. | TIBKAT | 1936

    Tests on aerofoil flaps in the compressed air tunnel

    Jones, R. / Bell, A. H. / Smyth, E. | SLUB | 1935
    Beteiligte: Jones, R. , Bell, A. H.

    Tests of six aerofoil sections at various Reynolds numbers in the Compressed Air Tunnel

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

    A comparison of the drag of trousered and retractable undercarriages

    Jones, R. / Bell, A. H. / Brown, A. F. | SLUB | 1936
    Beteiligte: Jones, R. , Bell, A. H. , Brown, A. F.

    Forced oscillations of aeroplanes, with special reference to von Schlippe's method predicting critical speeds for flutter

    Frazer, R. A. / Jones, William Neville Prichard | SLUB | 1936
    Beteiligte: Frazer, R. A. , Jones, William Neville Prichard

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

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

    Approximations to functions and to the solutions of differential equations

    Frazer, R. A. / Jones, William Neville Prichard / Skan, Sylvia W. | TIBKAT | 1937

    Tests on two streamline bodies in the compressed air tunnel

    Jones, R. / Williams, D. H. / Brown, A. F. | SLUB | 1937
    Beteiligte: 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
    Beteiligte: Frazer, R. A. , Jones, William Neville Prichard

    Theoretical stability and control characteristics of wings with various amounts of taper and twist

    Pearson, Henry A. / Jones, Robert T. | SLUB | 1938
    Beteiligte: Pearson, Henry A. , Jones, Robert T.

    Results of landing tests of various airplanes

    Hootman, J A / Jones, A R | NTRS | 1942

    Summary report on induction of water to inlet air as means of internal cooling in aircraft engine cylinders

    Rothrock, A.M. / Krsek, Jr., A. / Jones, A.W. | Engineering Index Backfile | 1942

    Changes Occurring in OILS and ENGINES from USE

    LINCOLN, BERT H. / SUESS, FRANK A. / BALDWIN, H. C. et al. | SAE Technical Papers | 1942