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Showing 10 out of a total of 11 results for community: School of Engineering (SoE).
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Application of the linear perturbation theory to compressible flow about bodies of revolution
Young, A. D.
;
Kirkby, S.
(
College of Aeronautics, Cranfield
,
1947-09
)
Note on the application of the linearised theory for compressible flow to transonic speeds
Robinson, A.
;
Young, A. D.
(
College of Aeronautics, Cranfield
,
1947-01
)
Technique of the step-by-step integration of ordinary differential equations
Duncan, W. J.
(
College of Aeronautics, Cranfield
,
1947-02
)
Source and vortex distributions in the linearised theory of steady supersonic flow
Robinson, A.
(
College of Aeronautics, Cranfield
,
1947-10
)
The effect of the sweepback of delta wings on the performance of an aircraft at supersonic speeds
Robinson, A.
;
Davies, F.T.
(
College of Aeronautics, Cranfield.
,
1947-03
)
Note on the dynamics of a slightly deformable body
Hemp, W. S.
(
College of Aeronautics, Cranfield
,
1947-02
)
Bound and trailing vortices in the linearised theory of supersonic flow, and the downwash in the wake of a delta wing
Robinson, A.
;
Hunter-Tod, J. H.
(
College of Aeronautics, Cranfield
,
1947-10
)
Wing body interference at supersonic speeds
Kirkby, S.
;
Robinson, A.
(
College of Aeronautics, Cranfield
,
1947-04
)
Note on the velocity and temperature distributions attained with suction on a flat plate of infinite extent in compressible flow
Young, A. D.
(
College Of Aeronautics, Cranfield
,
1947-08
)
The aerodynamic derivatives with respect to sideslip for a delta wing with small dihedral at supersonic speeds
Robinson, A.
;
Hunter-Tod, J. H.
(
College of Aeronautics
,
1947-12
)
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Author
Robinson, A. (6)
Young, A. D. (3)
Duncan, W. J. (2)
Hunter-Tod, J. H. (2)
Kirkby, S. (2)
Davies, F.T. (1)
Hemp, W. S. (1)
Date Issued
1947 (11)