Note / College of Aeronautics

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Körperschaft: Cranfield College of Aeronautics (VerfasserIn)
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Veröffentlicht: Cranfield 1954-
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Titel Jahr Band
Effect of body incidence on two afterbodies with a rearward facing jet 1992
Some experiments with fluidic devices in aviation kerosene 1969
Development of a 3-component strain-gauge for use on the Whirling Arm 1969
Calibration of the flow in the channel of the whirling arm 1969
The College of Aerodynamic Whirling Arm initial development tests 1967
Vortex tube performance data sheets 1967
Compounded normal modes of free vibration of cantilever plates 1967
Frequency response of an aircraft as determined from transient flight tests using the Fourier transformation method of analysis 1967
A design method for the dilution zones of gas turbine combustion chambers 1966
Studies in stability and control analysis of airframes having nonlinear aerodynamic characteristics 1966
Theoretical aspects of gas turbine combustion performance 1966
An advanced course in air transport engineering 1966
Aerodynamic characteristics of a 40 [degrees] swept back wing of aspect ratio 4.5 1965
Recent aeroelastic investigations at the College of Aeronautics 1965
Measurements of the moments of inertia of a Hawker Siddeley Dove Mk. 5 aircraft 1965
Slender shapes offering minimum drag in free-molecular flow : with an appendix on similarity law for longitudinal contours of optimum bodies in free-molecular flow 1965
On the flow along swept leading edges 1965
The teaching of aircraft design 1964
Tabulation of some layouts and virtual displacement fields in the theory of Michell optimum structures 1964
An investigation of surface deformations occurring at the contact edges of statically loaded discs 1964
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