M=2x0 to 2x7

von Cook, T. A.
Veröffentlicht in Supersonic wind tunnel tests on a 1/12th scale model of the Bristol type 188 research aircraft (1965)

The effects of ridge excrescences and trailing edge control gaps on twodimensional aerofoil characteristics

von Cook, T. A.
Veröffentlicht 19711972

Measurements of the boundary layer and wake of two aerofoil sections at high Reynolds numbers and high subsonic Mach numbers

von Cook, T. A.
Veröffentlicht 19711973

Wind tunnel measurements of the far-field pressures due to some lifting, slender Delta wings

von Cook, T. A.
Veröffentlicht 1965

Wind tunnel tests at Mach numbers up to 2.80 to determine the effects of changing spanwise volume distribution on slender, cambered ogee wing

von Cook, T. A.
Veröffentlicht 1965

Wind tunnel measurements at Mach numbers up to 2.80 of the effects of gulling on the longitudinal and lateral stability and drag of a cambered, slender ogee wing

von Cook, T. A.
Veröffentlicht 1965

Wind tunnel tests on a 1/12th scale model of the Bristol Type 188 research aircraft with rectangular, wedge intakes at machnumbers from 2.0 to 2.7

von Cook, T. A.
Veröffentlicht 1965

M=1x4 to 2x0

von Taylor, C. R.
Veröffentlicht in Supersonic wind tunnel tests on a 1/12th scale model of the Bristol type 188 research aircraft (1965)

Concentrated juice from fruits of small-fruited apple trees - As a semi-finished product for the food industry

von Kokh, D. A.
Veröffentlicht in International Conference on Food Science and Biotechnology (2021 : Jekaterinburg) International Conference on Food Science and Biotechnology (FSAB 2021) (2021)