CoA. Reports: Recent submissions

Now showing items 1-20 of 280

Addendum to type record. Avro "Lancaster" Mk.1 P. A. 474 Type record No. 1/P1/Lancaster. Investigation of boundary layer conditions on wings. M.O.S. Contract No.6/Aircraft/9807/C. B. 6(a)

College of Aeronautics, Department of Aircraft Design (College of Aeronautics, )
Temperature effects on material characteristics

Murphy, A. J.; Kennedy, A. J. (College of Aeronautics, )
A theoretical and experimental investigation of tail unit flutter on the M.S. 760 'Paris'

Mitchell, C. G. B.; Johns, D. J. (College of Aeronautics, )
Note on the limits to the local Mach number on an aerofoil in subsonic flow

Young, A. D. (College of Aeronautics, )
Multi-objective Tabu Search 2: first technical report

Tsotskas, Christos; Kipouros, Timoleon; Savill, Mark A. (Cranfield University, )
Experimental investigation on a cropped delta wing with edge blowing

Alexander, A. J. (College of Aeronautics, )
Experiments on a delta wing using leading edge blowing to remove the secondary separation

Alexander, A. J. (College of Aeronautics, )
Ignoration of distortional co-ordinates in the theory of stability and control

Duncan, W. J. (College of Aeronautics, )
Boundary layers with suction and injection a review of published work on skin friction

Craven, A. H. (College of Aeronautics, )
Skin friction in the laminar boundary layer in compressible flow

Young, A. D. (College of Aeronautics, )
Generic regional aircraft flying qualities for the approach and landing task

Gautrey, Jim (Cranfield University, )
Laplace plane GeoSAR feasibility study: summary of the group design project MSc in astronautics and space engineering 2014-15, Cranfield University

Hobbs, Stephen (Cranfield University, )
Measurement of the derivative 'ZW' for an oscillating aerofoil

Buchan, A. L.; Harris, K. D. (College of Aeronautics, )
On a theory of sandwich construction

Hemp, W. S. (College of Aeronautics, )
The elastic stability of sandwich plates

Hunter-Tod, J. H. (College of Aeronautics, )
Note on the limits to the local Mach number on an aerofoil in subsonic flow

Young, A. D. (College of Aeronautics, )
An improved law of cumulative damage in metal fatigue

Swanson, S. R. (College of Aeronautics, )
Aerodynamic characteristics of a swept wing with spanwise blowing.

Ayers, R. F.; Wilde, M. R. (Cranfield University, )
Buckling due to thermal stress of cylindrical shells subjected to axial temperature distributions

Johns, D. J.; Houghton, D. S.; Webber, J. P. H. (College of Aeronautics, )
Research at the College of Aeronautics Cranfield

Murphy, A. J. (College of Aeronautics, )

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