Advanced STOL turbo-prop powered transports |
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An aerodynamic investigation of a gas driven lift-cruise fan : part II |
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Annual report |
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Augmentor wing flight-test vechile program proposal: Volume III - Supporting Technical Data, DHC 67-22. |
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The Chipmunk primary trainer : designed to air force, army, navy and civil training requirements. |
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Correlation between theoretical and experimental pressure distributions on vane-type double and triple-slotted flaps |
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Le Dash 7 : avion de ligne stol et silencieux. |
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The De Havilland Canada story, c1983: |
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The De Havilland war worker |
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Defence industrial research program, STOL operations : program A-7 : progress report. |
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DHC-3 king beaver : model specification. |
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DHC-5 buffalo for military service. |
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Drag rise characteristics of STOL transport configurations |
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The effects of ground surface grids on the lift characteristics of a jet VTOL model |
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Gust response of STOL aircraft : interim report, A-13 : covering period June 1, 1967 to October 31, 1968. |
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De Havilland Chipmunk |
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An investigation of the effect of secondary inlet area on the pressure in an ejector |
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Lateral handling qualities of small aircraft : program A-12. |
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Low speed wind tunnel tests of a NACA 16-309 airfoil with trailing-edge flap |
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The oscillating jet thrust augmentor - early development at De Havilland Aircraft of Canada, 1964-1965 |
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Parts list for the De Havilland Gipsy Major IC, Aero Engine. |
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Preliminary analysis of a two-dimensional thrust augmentor with jet-enclosed mixing region |
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Profile drag measurements on 2-dimensional high lift wing models |
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Progress report submitted in fulfilment of D.R.B. S.T.O.L. utility aircraft design study. |
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Rapp. annu. (Corp. dév. invest. Can.) |
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Rapport annuel |
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A rational wing box weight estimation technique |
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Report on the phase 3 tests of the DHC augmentor-wing model in the 40 x 80 foot wind tunnel at the Ames Research Center NASA 1967 : volume II |
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Resumé of operations. |
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Slipstream deflection and wing interference studies : program A-14. |
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Specification for wind tunnel tests of VTOL model WTAZ at NAE, Ottawa, 1967 |
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Static tests of a sonic oscillator |
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Static tests of a two-dimensional external augmentor VTOL model, 1965 |
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Steady state lateral stability analysis of an augmentor-wing transport |
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STOL aircraft powered by fan engines |
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STOL transportation systems planning. |
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A study of the duct system performance and requirements of several VTOL fan lift/cruise aircraft configurations |
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Supplement no. 1 to DHC 70-20, Propulsion system design review data: Augmentor - wing flight test vechicle (Buffalo-spey conversion), presented at design review meeting March 1971. |
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Tests of a full scale section of the Ames model augmentor configuration in the Aerodynamics Test Laboratory, Malton |
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A theoretical viscous mixing approach to two-dimensional and axisymmetrical central jet augmentors with straight walled diffusers |
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They are talking about us again! : 1928-1968, fortieth year |
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Trade catalogues (NLC), Transportation |
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The Trident 2 in Canada. |
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Twin turbo-fan aircraft design study |
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Two-dimensional high lift B. L. C. wind tunnel tests (part II) test period (January 1966) |
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The U.A.W.-C.I.O. war worker |
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Wing augmentor research program : Dir Project A-2 : progress report. |
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