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Showing 10 out of a total of 95 results for collection: CoA. Reports.
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The effect of vibrations (sonic and subsonic frequencies) during the period of solidification on the mechanical properties of castings of gas turbine materials with special reference to H. R. Crown Max and Nimonic C. 75
Jagaciak, Jerzy
(
College of Aeronautics, Cranfield.
,
1955-09
)
The use of a potential flow tank for testing axi-symmetric contraction shapes suitable for wind tunnels
Babister, A. W.
;
Marshall, W. S. D.
;
Lilley, G. M.
;
Sills, E. C.
;
Deards, S. R.
(
College of Aeronautics, Cranfield.
,
1951-04
)
Measurement of the derivative 'ZW' for an oscillating aerofoil
Buchan, A. L.
;
Harris, K. D.
(
College of Aeronautics
,
1950-06
)
Note on the development of a trailing-edge flap as a stall-detector
Bethwaite, C. F.
(
College of Aeronautics, Cranfield
,
1953-09
)
The numerical solution of certain differential equations occurring in Crocco's theory of the laminar boundary layer
Kirkby, S.
;
Nonweiler, T.
(
College of Aeronautics, Cranfield
,
1953-05
)
On some aspects of the noise propagation from supersonic aircraft
Lilley, G. M.
;
Westley, R.
;
Yates, A. H.
;
Busing, J. R.
(
College of Aeronautics, Cranfield
,
1953-02
)
The calculation of the profile drag of aerofoils and bodies of revolution at supersonic speeds
Young, A. D.
(
College of Aeronautics, Cranfield
,
1953-04
)
Estimation of the effects of distortion on longitudinal stability of swept wing aircraft at high speeds (sub-critical mach numbers)
Campion, B. S.
(
College of Aeronautics, Cranfield
,
1954-01
)
A note on the estimation of some low speed characteristics of delta wings
Rose, R. G.
(
College of Aeronautics, Cranfield
,
1953-01
)
The two-dimensional laminar boundary layer at hypersonic speeds
Nonweiler, T.
(
College of Aeronautics, Cranfield
,
1953-01
)
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Nonweiler, T. (9)
Howe, D. (5)
Lilley, G. M. (5)
Craven, A. H. (4)
Marshall, W. S. D. (4)
Radok, J. R. M. (4)
Westley, R. (4)
Babister, A. W. (3)
Bethwaite, C. F. (3)
Goodger, E. M. (3)
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