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    Die Flösserei im Stromgebiet der Weser

    Delfs, Jürgen | TIBKAT | 1952

      Die Flösserei im Stromgebiet der Weser

      Delfs, Jürgen | GWLB - Gottfried Wilhelm Leibniz Bibliothek | 1952

    Bibliography of NACA papers on rotating-wing aircraft, January 1952

    Gessow, Alfred | TIBKAT | 1952

    Impingement of water droplets on an NACA 65 1-212 airfoil at an angle of attack of 4°

    Brun, Rinaldo J. / Serafini, John S. / Moshos, George J. | TIBKAT | 1952

    Measurements of aerodynamic heating obtained during demonstration flight tests of the Douglas D-558-II airplane

    Jones, Ira P. | TIBKAT | 1952

    Wide angle diffusers employing boundary layer control

    Manoni, L. R. | TIBKAT | 1952

    Experiments giving hinge moment and lift on a NACA 0015 aerofoil fitted with a 40 per cent control, with especial reference to effect of curvature of control surface

    Batson, A. S. / Preston, J. H. / Warsap, J. H. et al. | TIBKAT | 1952

    Tests in the compressed air tunnel on the aerofoils NACA 0015 and NACA 0030 with and without split flap and other aerofoils of various thickness with a split flap

    Jones, R. | TIBKAT | 1952

    Preliminary experimental investigation of the flight of a person supported by a jet thrust device attached to his feet

    Zimmermann, C. H. / Hill, Paul R. / Kennedy, T. L. | TIBKAT | 1953

    NACA 65-series compressor rotor performance with varying annulus-area ratio, solidity, blade angle, and Reynolds number and comparison with cascade results

    Schulze, Wallace M. / Erwin, John R. / Ashby, George C. | TIBKAT | 1953

    A transonic wind-tunnel investigation of the longitudinal stability and control characteristics of a 0.09-scale model of the Bell X-5 research airplane and comparison with flight

    Bielat, Ralph P. / Campbell, George S. | TIBKAT | 1953

    Fuselage pressures measured on the Bell X-1 research airplane in transonic flight

    Knapp, Ronald J. / Jordan, Gareth H. / Johnson, Wallace E. | TIBKAT | 1953

    Flight measurements of pressures on base and rear part of fuselage of the Bell X-1 research airplane at transonic speeds, including power effects

    Knapp, Ronald J. / Johnson, Wallace E. | TIBKAT | 1953

    High-speed tunnel tests of a 5 per cent. chord dive-recovery flap on a NACA 0015 aerofoil

    Clarke, D. A. | TIBKAT | 1953

    Flight measurements of average skin-friction coefficients on a parabolic body of revolution (NACA RM-10) at Mach numbers from 1.0 to 3.7

    Loposer, J. Dan / Rumsey, Charles B. | TIBKAT | 1954

    Influence of aeroplane characteristics on response to gusts of various forms

    Hooke, F.H. | Engineering Index Backfile | 1954

    Further experiments on an NACA 23021 aerofoil with a 15 per cent handley page slotted flap in the compressed air tunnel

    Jones, R. / Bell, A. H. | TIBKAT | 1954

    24-ft wind tunnel tests on a propeller with NACA 16 series sections : test results and analysis into mean lift-drag data

    MacDougall, A. R. C. / Haines, A. B. | TIBKAT | 1954

    Flight tests of a delta-wing vertically rising airplane model powered by a ducted fan

    Lovell, Powell M. | TIBKAT | 1955

    Wind-tunnel tests on the NACA 63A009 aerofoil with distributed suction over the nose

    Gregory, Nigel | TIBKAT | 1955

    Einige Forschungsarbeiten aus der Gasturbinentechnik

    Leist, Karl | TIBKAT | 1956

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