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Browsing Aeronautical Research Council by Author "R. J. Monaghan"

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An approximate solution of the compressible laminar boundary layer on a flat plate

R. J. Monaghan (1949)

Following a major assumption that enthalpy and velocity are dependent only on local conditions, an enthalpy-velocity relation ... is obtained for the laminar boundary layer on a flat plate where subscripts p refer to the ...
Boundary-layer measurements on 15-deg and 24.5-deg cones at small angles of incidence at M = 3.17 and 3.82 and zero heat transfer

F. V. Davies; R. J. Monaghan (1957)

Transition measurements on 15-deg and 24.5-deg cones at MCD = 3.17 and 3.82 showed that the transition front was extremely sensitive to incidence, a fourfold variation occurring between transition Reynolds numbers on the ...
Comparison between experimental measurements and a suggested formula for the variation of turbulent skin-friction in compressible flow

R. J. Monaghan (1951)
Effects of heat transfer on laminar boundary-layer development under pressure gradients in compressible flow

R. J. Monaghan (1960)

Under review
Formulae and approximations for aerodynamic heating rates in high speed flight

R. J. Monaghan (1957)
Formulae for estimating the forces in seaplane-water impacts without rotation or chine immersion

R. J. Monaghan; P. R. Crewe (1949)

This report presents formulae and curves for estimating the maximum forces, together with the times and drafts associated with these forces, in main-step landings of seaplanes, provided that there is no rotation and that ...
The measurement of heat transfer and skin friction at supersonic speeds part 2 boundary layer measurements on a flat plate at M = 2.5 and zero heat transfer

R. J. Monaghan; J. E. Johnson (1952)
The measurement of heat transfer and skin friction at supersonic speeds part 3 measurements of overall heat transfer and of the associated boundary layers on a flat plate at Ml = 2.43

R. J. Monaghan; J. R. Cooke (1953)
The measurement of heat transfer and skin friction at supersonic speeds part 4 tests on a flat plate at M = 2.82

R. J. Monaghan; J. R. Cooke (1953)
Measurements of the effect of surface cooling on boundary layer transition on a 15 degrees cone part 1 tests at M = 2 and 3 in an 8 in. x 9 in. wind tunnel at R.A.E./Bedford

A. C. Browning; J. F. W. Crane; R. J. Monaghan (1958)
A review and assessment of various formulae for turbulent skin friction in compressible flow

R. J. Monaghan (1953)
A review of the essentials of impact force theories for seaplanes and suggestions for approximate design formulae

R. J. Monaghan (1947)

Classical theories of impact of seaplanes on water have been based on the assumption of a transfer of momentum to a hypothetical associated mass of water attached to the seaplane, such that the total momentum of the two ...
A survey and correlation of data on heat transfer by forced convection at supersonic speeds

R. J. Monaghan (1953)

This report surveys and, wherever possible, correlates experimental data available in the united Kingdom up to January 1953 on heat transfer by forced convection to bodies moving through the air at supersonic speeds (or ...
A theoretical examination of the effect of deadrise on wetted area and associated mass in seaplane-water impacts

R. J. Monaghan (1949)

A theoretical examination is made of the deadrise effect on associated mass and wetted area in the two-dimensional impact case (vertical drop of an infinitely long wedge at zero attitude). Available estimates are summarised ...
The use of pitot-tubes in the measurement of laminar boundary

R. J. Monaghan (1955)

Consideration of experimental results obtained with relatively large pitot-tubes in relatively thin laminar boundary layers on cones and flat plates in supersonic wind tunnels and then analysed using standard pitot equations, ...

Browsing Aeronautical Research Council by Author "R. J. Monaghan"

Browsing Aeronautical Research Council by Author "R. J. Monaghan"

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