D. I. A. Poll

发表

A New Hypothesis for Transition on the Windward Face of the Space Shuttle

D. I. A. Poll, 1986 .

Aerospace and the environment what contribution can aerodynamics make

D. I. A. Poll, 2000 .

Annual Review of Fluid Mechanics, Vol. 19. 1987. Lumley J. L.et al. (Editors). Annual Reviews, Inc., Palo Alto. 1987. 626pp. Illustrated. $35.00.

D. I. A. Poll, 1988 .

21st-Century civil aviation: Is it on course or is it over-confident and complacent? – thoughts on the conundrum of aviation and the environment

D. I. A. Poll, D. Poll, 2017, The Aeronautical Journal.

A first order method for the determination of the leading mass characteristics of civil transport aircraft

D. I. A. Poll, 2011 .

Spiral vortex flow over a swept-back wing

D. I. A. Poll, 1986, The Aeronautical Journal (1968).

SLENDER FOREBODY AERODYNAMICS AT HIGH ALPHA

D. I. A. Poll, K. Petterson, D. Poll, 2000 .

A Parallel Processing Approach to Transition Prediction for Laminar Flow Control System Design

Rupert W. Ford, D. I. A. Poll, 1995, Sci. Program..

The optimum aeroplane and beyond

D. I. A. Poll, D. Poll, 2009, The Aeronautical Journal (1968).

On the effect of uniform suction on stability and transition in zero pressure gradient viscous incompressible flow

D. I. A. Poll, S. A. Walsh, M. C. Gallagher, 1996 .

On the effect of stage length on the efficiency of air transport

D. I. A. Poll, 2011 .

Implications of 3-D transition mechanisms on the performances of space vehicles

D. I. A. Poll, 1995 .

Experimental and computational investigation of leading edge transition at Mach 1.6

D. I. A. Poll, Colin Coleman, Ray-Sing Line, 1997 .

Effect of curvature on three-dimensional boundary-layer stability

M. R. Malik, D. I. A. Poll, M. Malik, 1985 .

Some aspects of the flow near a swept attachment line with particular referenceto boundary layer transition

D. I. A. Poll, 1978 .

On the stability of an infinite swept attachment line boundary layer

M. R. Malik, D. I. A. Poll, Philip Hall, 1984, Proceedings of the Royal Society of London. A. Mathematical and Physical Sciences.

On the effect of wing taper and sweep direction on leading edge transition

D. J. Paisley, D. I. A. Poll, D. Poll, 1985, The Aeronautical Journal (1968).

Leading edge transition on a 76 degree swept cylinder at Mach 1.6

Stephen W. D. Wolf, James A. Laub, D. I. A. Poll, 1996 .

Assessment of the eN Method as a Transition Prediction Tool for Zero Pressure Gradient Flows with and without Boundary Layer Suction

D. I. A. Poll, J. E. Ellis, S. A. Walsh, 2001 .

On the effects of boundary-layer transition on a cylindrical afterbody at incidence in low-speed flow

D. I. A. Poll, D. Poll, 1985, The Aeronautical Journal (1968).

Three-Dimensional Boundary Layer Transition via the Mechanisms of “Attachment Line Contamination” and “Cross Flow Instability”

D. I. A. Poll, 1980 .

On the stability of an infinite swept attachment line boundary layer

D. I. A. Poll, Mujeeb R. Malik, Philip Hall, 1984 .

Some observations of the transition process on the windward face of a long yawed cylinder

D. I. A. Poll, D. Poll, I. Poll, 1985, Journal of Fluid Mechanics.

Relaminarisation of the Swept Wing Attachment-Line by Surface Suction

D. I. A. Poll, D. Poll, M. Danks, 1995 .