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Mechanical aspects of turbine blade cooling.

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Bibliographic Details
Corporate Author:	Aeronautical Research Council (Great Britain)
Other Authors:	Waldren, N. E.
Format:	Book
Language:	English
Published:	London : H.M.S.O., 1965.
Series:	Reports and memoranda (Aeronautical Research Council (Great Britain)) ; no. 3404.
Subjects:	Turbines > Blades > Cooling.

Norlin Library - Basement - Government Information - Foreign

Holdings details from Norlin Library - Basement - Government Information - Foreign
Call Number:	301-Ae8 4:3399
301-Ae8 4:3399 (3399-3416 1965)	Available Place a Hold Contents The following works are all found in the book indicated by the call number above. An experimental high-temperature turbine (No. 126) / by D.E Fray and J.F. Barnes. Forces on aerofoils with both incidence and forward speed varying / by D.G. Randall. Stress-concentration factors for rounded rectangular holes in infinite sheets / by A.... Calculation of unsteady generalised air-forces on a thin wing oscillating harmonicall... A theory of the blockage effects on bluff bodies and stalled wings in a closed wind t... Mechanical aspects of turbine blade cooling. Transonic compressor noise : the effect of inlet guide vane/rotor spacing / by D.A. K... An investigation of the flow about circular cylinders placed normal to a low-density,... The calculation of lateral stability derivatives of slender wings at incidence, inclu... The supersonic flow past a circular cone at incidence / by B.A. Woods. Structural damage caused by impulsive loads: a theoretical analysis / by E.H. Mansfie... A wind-tunnel investigation of the directional and longitudinal stability of the Jave... Reports and memoranda / Aeronautical Research Council. Lift due to interference between an aerofoil and an external non-lifting body / by S.... Oscillatory aerodynamic forces in linearised supersonic flow for arbitrary frequencie... Turbulent flow past two-dimensional bases in supersonic streams / by R.C. Hastings. Some exploratory measurements of leading-edge vortex positions on a delta wing oscill... Design of warped slender wings with the attachment line along the leading edge / by J...