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AERONAUTICAL RESEARCH COUNCIL
Books by AERONAUTICAL RESEARCH COUNCIL
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Regenerator heat exchangers for gas-turbines
AERONAUTICAL RESEARCH COUNCIL
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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 (Reports & memoranda series;no.2698)
Aeronautical Research Council
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Porous properties of various materials liable to be used for making parachutes (Current papers series;no.24)
Aeronautical Research Council
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The relative strength and stiffness properties required for strut materials (Reports and memoranda series;no.2490)
Aeronautical Research Council
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Sandwich construction and core materials (Reports & memoranda series)
Aeronautical Research Council
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Wind tunnel tests on the spoiling effects of engine cooling gills on radial air-cooled installations on a wing (Reports & memoranda series;no.2558)
Aeronautical Research Council
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Binary aileron-spring-tab flutter (Reports and memoranda series;no.2576)
Aeronautical Research Council
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Revised high-speed lift and drag data for Clark Y sections for propeller performance calculations (Reports and memoranda series;no.2474)
Aeronautical Research Council
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Tables of characteristics slopes for use in the design of nozzles for supersonic wind tunnels (Current papers; no.337)
Aeronautical Research Council
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The design and testing of supersonic nozzles (Reports & memoranda series;no.2712)
Aeronautical Research Council
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Low-speed wind tunnel investigation of the change in aero-dynamic centre position and in C/m/o due to propeller turbine nacelles (Current papers series;no.13185)
AERONAUTICAL RESEARCH COUNCIL
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Some high-speed tests on turbine cascades (Reports & memoranda series;no.2697)
Aeronautical Research Council
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Chemical solids as diffusible coating films for visual indications of boundary-layer transition in air and water (Reports & memoranda series;no.2755)
Aeronautical Research Council
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Wind tunnel tests at mach numbers up to 1, 8 on a model with 1, 36 scale wings and nacelles of a twin-engined supersonic aircraft (Bristol 188) (Current papers; no.798)
Aeronautical Research Council
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A free-flight investigation into the effect of body shaping on the zero-lift drag of a wing-body combination at transonic and supersonic speeds (Reports & memoranda;no.3193)
Aeronautical Research Council
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Some advantages and disadvantages of variable and non-linear gearing between the pilot's control and the control surfaces (Current papers;no.263)
Aeronautical Research Council
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Experiments on two-dimensional base flow at M-2.4 (Reports & memoranda; no.3064)
Aeronautical Research Council
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Note on the effect of compressibility on the profile drag of aerofoils at subsonic mach numbers in the absence of shock waves (Reports and memoranda series;no.2400)
Aeronautical Research Council
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Calculations of the thermodynamic properties of nitrogen at high pressures: By J.L. Wilson and J.D. Regan (Current papers;no.771)
Aeronautical Research Council
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A survey of performance reduction with particular reference to turbo-propeller aircraft (Reports and memoranda series;no.2757)
Aeronautical Research Council
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A series of low-drag aerofoils embodying a new camber-line (Reports & memoranda series;no.2494)
Aeronautical Research Council
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The two-dimensional subsonic flow of an inviscid fluid about an aerofoil of arbitrary shape (Reports & memoranda series;no.2811)
Aeronautical Research Council
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Free-flight experiments on the measurement of free-stream static pressure at transonic speeds with particular reference to theMk.9 pitot-static head (Current papers no.475)
Aeronautical Research Council
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Measurement of aircraft attitude relative to flight path during dives (Reports & memoranda series;no.2564)
Aeronautical Research Council
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Flutter of an untapered wing allowing for thermal effects (Current papers;no.442)
Aeronautical Research Council
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Wind-tunnel tests on the Supermarine S.24/37,a high-wing monoplane with a variable-incidence wing (Reports and memoranda series;mo.2451)
Aeronautical Research Council
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Wind-tunnel tests on the prevention of boundary-layer separation by distribution suction at the rear of a thick aerofoil (NPL 153) (Reports & memoranda series;no.2788)
Aeronautical Research Council
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Wind tunnel measurements of the far-field pressures due to some lifting, slender delta wings (Current papers; no.802)
Aeronautical Research Council
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