John T. Conway

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Professor John T. Conway PhD, MSc Kontor: Rom D3-036, Campus Grimstad Email: john.conway@uia.no Tlf: 3723 3267 Adresse: Fakultet for Teknologi og Realfag, Universitetet i Agder, Grimstad

Bakgrunn

2001-: Professor ved Universitetet i Agder
2001: Ph.D. (Anvendt Matematikk), Cambridge University (King's College)
1992-: Dosent ved Høgskolen i Agder
1986-1992: Universitetslektor ved Universitetet i Montreal, Kanada
1982-1985: Ingeniør, British Aerospace, Bristol, UK
1982: M.Sc. (Aerodynamikk), Cranfield University (College of Aeronautics)
1978, 1981: B.A., M.A. (Fysikk), Cambridge University (King's College)

Undervisning

Tidsskriftsartikler

(J21) J. T. Conway, "Fourier series for elliptic integrals and some generalizations via hypergeometric series", J. Integral Transforms Spec. Funct., Vol. 19, No. 5, pp. 305-315, 2008.

(J20) J. T. Conway, "Calculations for a disk source and a general detector using a radiation vector potential", Nucl. Instr. and Meth. Phys. Res. A, Vol. 589, pp. 20-33, 2008.

(J19) J. T. Conway, "Noncoaxial Inductance Calculations Without the Vector Potential for Axisymmetric Coils and Planar Coils", IEEE Trans. Magn., Vol. 44, No. 4, pp. 453-462, 2008.

(J18) J. T. Conway,"Geometric efficiency for a parallel-surface source and detector system with at least one axisymmetric surface", Nucl. Instr. and Meth. Phys. Res. A, Vol. 583, pp. 382-393, 2007.

(J17) J. T. Conway, "Fourier and other series containing associated Legendre functions for incomplete Epstein-Hubbell integrals and functions related to elliptic integrals", J. Integral Transforms Spec. Funct., Vol. 18, No. 3, pp. 179-191, 2007.

(J16) J. T. Conway,"Inductance Calculations for Noncoaxoal Coils Using Bessel Functions", IEEE Trans. Magn., Vol. 43, No. 3, pp. 1023-1034, 2007.

(J15) J. T. Conway,"Fourier series for the Legendre elliptric integrals", J. Integral Transforms Spec. Funct., Vol. 17, No. 7, pp. 499-505, 2006.

(J14) J. T. Conway,"Generalizations of Ruby's formula for the geometric efficiency of a parallel-disk source and detector system", Nucl. Instr. and Meth. Phys. Res. A, Vol. 562, pp. 146-153, 2006.

(J13) J. T. Conway, "Trigonometric integrals for the magnetic field of the coil of rectangular cross-section", IEEE Trans. Magn., Vol. 42, No. 5, pp. 1538-1548, 2006.

(J12) J. T. Conway, "Epstein-Hubbell Integrals Regarded as Legendre Functions of the Second Kind", J. Radiation Physics and Chemistry, 2006.

(J11) J. T. Conway, "New Exact Solution Procedure for the Near Fields of the General Thin Circular Loop Antenna", IEEE Trans. Antennas and Propagation, Vol. 54, pp. 509-517, 2005.

(J10) J.T. Conway and J. Su, "PMAL Flow Calculations for the Aurora Aircraft using Non-Axisymmetric Propeller Actuator Disks", CASI J., Vol. 49, No. 1., pp. 1-9, 2003.

(J9) J.T. Conway, "Exact Solutions for the Magnetic Fields of Axisymmetric Solenoids and Current Distributions", IEEE Trans. Magn., Vol. 37, No. 4, pp. 2977-2988, 2001.

(J8) J. Su and J.T. Conway, "Numerical Analysis of the Aerodynamics of the AURORA Aircraft by an Inviscid/Viscous Interaction Method", CASI J., Vol. 47, No. 1, pp. 17-24, 2001.

(J7) A.P. Schaffarczyk and J.T. Conway, "Comparison of a Nonlinear Actuator Disk Theory with Numerical Integration Including Viscous Effects", CASI J., Vol. 46, No. 4, pp. 209-215, 2000.

(J6) J.T. Conway, "Analytical Solutions for the Newtonian Gravitational Field Induced by Matter Within Axisymmetric Boundaries", Mon. Not. R. Astron. Soc., Vol. 316, No. 3, pp. 540-554, 2000.

(J5) J.T. Conway, "Exact Solutions for the Gravitational Potential of a Family of Heterogeneous Spheroids", Mon. Not. R. Astron. Soc.,Vol. 316, No. 3, 555-558, 2000.

(J4) J.T. Conway and J. Su, "PMAL Propeller-Induced Asymmetric Flow Calculations for the Aurora Aircraft Using Embedded Nonlinear Actuator Disks", CASI J., Vol. 46, No. 1, pp. 20-27, 2000.

(J3) J.T. Conway, "Prediction of the Performance of Heavily Loaded Propellers With Slipstream Contraction", CASI J., Vol. 44, pp. 169-174, 1998.

(J2) J.T. Conway, "Exact Actuator Disk Solutions for Non-uniform Heavy Loading and Slipstream Contraction", J. Fluid Mech., Vol. 365, pp. 235-267, 1998.

(J1) J.T. Conway, "Analytical Solutions for the Actuator Disk with Variable Radial Distribution of Load", J. Fluid Mech., Vol. 297, pp. 327-355, 1995.

Konferanseartikler

(C16) J. T. Conway, "Cylindrical Green's Function Approach for Wind Turbines and Related Applications", NREL Conference, IEA Annexes XX and XI, Montreal, Quebec, Canada, June 17th, 2004.

(C15) J. T. Conway, "Analytical Solutions for the General Non-axisymmetric Linearized Actuator Disk", AIAA Paper 2003-3521, 21st AIAA Applied Aerodynamics Conference, Orlando, Florida, June 23-26, 2003.

(C14) J. T. Conway and A. P. Schaffarczyk, "Comparison of Actuator Disk Theory with Navier-Stokes Calculations for a Yawed Actuator Disk", 8th CASI Aerodynamics Symposium, Montreal, April 28-30, 2003.

(C13) J. T. Conway, "Application of an Exact Nonlinear Actuator Disk Theory to Wind Turbines", ICNPAA 2002 - 4th International Conference on Nonlinear Problems in Aviation and Aerospace, Melbourne, Florida , May 15-17, 2002.

(C12) J.T. Conway and J. Su, "PMAL Flow Calculations for the Aurora Aircraft using Non-Axisymmetric Propeller Actuator Disks", 8th CASI Aerodynamics Symposium, Toronto, Ontario, Canada, April 29 - May 2, 2001.

(C11) A. P. Schaffarczyk and J.T. Conway, "Application of a Nonlinear Actuator Disk Theory to Wind Turbines", 14th Symposium IEA Joint Action on Aerodynamics of Wind Turbines, NREL, Boulder, Colorado, Dec 4, 2000.

(C10) J. Su and J.T. Conway, "Numerical Analysis of the Aerodynamics of the AURORA Aircraft by an Inviscid/Viscous Interaction Method", 22nd ICAS Congress, Harrogate, United Kingdom, August 28-31, 2000.

(C9) J.T. Conway and F. Tezok, "Application of the CANAERO Unsteady Panel Method to Oscillating Wings", ICNPAA 2000 - 3rd International Conference on Nonlinear Problems in Aviation and Aerospace, Daytona Beach, Florida , May 10-12, 2000.

(C8) J.T. Conway and F. Tezok, "A Time-Marching Scheme for the CANAERO Three-Dimensional Vortex Sheets Panel Method", AIAA Paper 2000-0791, 38th Aerospace Sciences Meeting & Exhibit, Reno, Nevada, January 10-13, 2000.

(C7) J.T. Conway and J. Su, "PMAL Propeller-Induced Asymmetric Flow Calculations for the Aurora Aircraft Using Embedded Nonlinear Actuator Disks", CASI 7th Aerodynamics Symposium, Montreal, Quebec, Canada, May 2-5, 1999.

(C6) J.T. Conway, "Prediction of the Performance of Heavily Loaded Propellers With Slipstream Contraction", CASI 6th Aerodynamics Symposium, Toronto, Canada, April 28-30, 1997.

(C5) F. Tezok and J. Conway, "Calculation of Unsteady Incompressible Inviscid Flow about Wings and Bodies using CANAERO-T Panel Method", 4th CASI Aerodynamics Symposium, Ottawa, Canada, May 3-4, 1993.

(C4) M. Mackay and J.T. Conway, "Modelling the Crossflow Body Separation on a Submarine using a Panel Method", Warship 91, International Symposium on Naval Submarines 3, London, United Kindom, May 13-15, 1991.

(C3) J.T. Conway and M. Mackay, "Prediction of the Effects of Body Separation Vortices on Submarine Configurations Using the CANAERO Panel Method", AIAA Paper 90-0302, 28th Aerospace Sciences Meeting, Reno, Nevada, January 8-11, 1990.

(C2) J.T. Conway, "Modelling of Boundary Layer and Trailing Edge Thickness Effects for the Euler Equations Using Surface Transpiration", 1st Canadian Symposium on Aerodynamics, Ottawa, Ontario, Canada, Dec 4-5, 1989.

(C1) J. T. Conway and F. Mavriplis, "CANAERO - A Low Order Panel Method With Wake-Relaxation and Boundary Layer Effects", CASI 34th Annual General Meeting, Toronto, Ontario, Canada, May 25-26, 1987.

Industrielle Rapporter

(R32) F. Tezok and J. T. Conway, "Proposal For The Canaero Computer Code to Include Free-surface Effects and Further Developments of the Time-stepping Capability", Canadair Report RAZ-000-562, Montreal, Quebec, Canada, December 1991.

(R31) J. T. Conway and F. Tezok, "Final Report on the Further Development of the CANAERO Computer Code to Include a Time-stepping Capability", Canadair Report RAZ-000-563, Montreal, Quebec, Canada, October 1991.

(R30) J. T. Conway, "First Quarterly Progress Report on the Further Development of the CANAERO Computer Code to Include a Time-stepping Capability", Canadair Report RAZ-000-555, Montreal, Quebec, Canada, January 1991.

(R29) J. T. Conway, "MDRAG Calculations for RJ and CL601 Horizontal Tail Ice Accretion Shapes", Canadair Report MAA-000-189, Montreal, Quebec, Canada, November 1990.

(R28) J. T. Conway, "FLO82BL 2-Dimensional Euler Code with Viscous-Inviscid Interaction Using Surface Transpiration - User Manual", Canadair Report MAA-000-174, Montreal, Quebec, Canada, November 1990.

(R27) J. T. Conway and F. Kafyeke, "Development of Advanced CFD Methods for Analysis and Design of Aircraft Aerodynamic Configurations", DIR Project 22078EH01 First Milestone Report, Canadair Report RAZ-000-549, Montreal, Quebec, Canada, April 1990.

(R26) J. T. Conway, "Further Development of the CANAERO Computer Code to Include Propulsor Modelling, Final Report", Canadair Report RAZ-000-548, Montreal, Quebec, Canada, March 1990.

(R25) J. T. Conway, "A proposal for the Further Development of the CANAERO Computer Code to Include Propulsor Modelling and a Time-stepping Capability", Canadair Report RAZ-000-545, Montreal, Quebec, Canada, March 1989.

(R24) J. T. Conway, "Enhancement of the CANAERO Computer Program to Include Body Separation Vortices, Final Report in 2 Volumes. (Vol. 1: Unclassified, Vol. 2: Restricted)", Canadair Report RAZ-000-536, Montreal, Quebec, Canada, April 1988.

(R23) J. T. Conway, "Canadair Computer Program Enhancement to Include Body Separation Vortices, Progress Report No. 5", Canadair Report RAZ-000-535, Montreal, Quebec, Canada, March 1988.

(R22) J. T. Conway, "Canadair Computer Program Enhancement to Include Body Separation Vortices, Progress Report No. 4 (Restricted)", Canadair Report RAZ-000-534, Montreal, Quebec, Canada, January 1988.

(R21) J. T. Conway, "Proposal for the Development of the CANAERO Panel Method for Marine Propeller Analysis", Canadair Report RAZ-000-531, Montreal, Quebec, Canada, October 1987.

(R20) J. T. Conway, "Canadair Computer Program Enhancement to Include Body Separation Vortices, Progress Report No. 3", Canadair Report RAZ-000-529, Montreal, Quebec, Canada, September 1987.

(R19) J. T. Conway, "Canadair Computer Program Enhancement to Include Body Separation Vortices, Progress Report No. 2", Canadair Report MAA-000-115, Montreal, Quebec, Canada, July 1987.

(R18) J. T. Conway, "Canadair Computer Program Enhancement to Include Body Separation Vortices, Progress Report No. 1", Canadair Report MAA-000-112, Montreal, Quebec, Canada, April 1987.

(R17) J. T. Conway, "Proposal for the Enhancement of the CANAERO Computer Program to Include Body Separation Vortices", Canadair Report RAZ-000-521, Montreal, Quebec, Canada, November 1986.

(R16) J. T. Conway and P. Piperni, "Unsolicited Proposal (Preliminary) for Further Development of CANAERO to Include Time-stepping and Free-surface Effects", Canadair Report RAZ-000-520, Montreal, Quebec, Canada, October 1986.

(R15) J. T. Conway, "CANAERO III Development to Include Wake Relaxation and Vortex Roll-up, Final Report", Canadair Report RAZ-000-519, Montreal, Quebec, Canada, June 1986.

(R14) J. T. Conway, "CANAERO III Development to Include Wake Relaxation and Vortex Roll-up, Progress Report No. 3", Canadair Report RAZ-000-515, Montreal, Quebec, Canada, April 1986.

(R13) J. T. Conway, "CANAERO III Development to Include Wake Relaxation and Vortex Roll-up, Progress Report No. 2", Canadair Report RAZ-000-511, Montreal, Quebec, Canada, October 1985.

(R12) J. T. Conway, "Vertical Launch Seawolf: Effect of Boost Cable Ducts on Boosted Configuration Aerodynamics", British Aerospace Report BT 18122 (Restricted), Bristol, United Kingdom, May 1985.

(R11) J. T. Conway, "The Effect of Reynolds Number on the Aerodynamics of the Boosted Vertical Launch Seawolf Missile Configuration", British Aerospace Report BT 18094 (Company Confidential), Bristol, United Kingdom, January 1985.

(R10) L. D. Miller and J. T. Conway, "Efflux Problems in Confined Spaces: The Case for Tube Launched Missiles, Discussion Document", British Aerospace Report BT 17399 (Company Confidential), Bristol, United Kingdom, January 1985.

(R9) J. T. Conway, W. D. Davies and G. Beaman, "Initial Assessment of the Out-of-Plane Vertical Launch Seawolf Wind Tunnel Data from the 13' x 9' Bedford Tunnel", British Aerospace Reports BT 14655 and 255/JTC/VLSW/607 (Confidential), Bristol, United Kingdom, December 1984.

(R8) L. D. Miller & J. T. Conway, "Vertical Launch Seawolf: Phaze 1 Separation Unit Trials Data Report", British Aerospace Report BT 16962 (Confidential), Bristol, United Kingdom, September 1984.

(R7) J. T. Conway, "Vertical Launch Seawolf: Separation Unit Gas Dynamic Model", British Aerospace Report BT 16963 (Confidential), Bristol, United Kingdom, September 1984.

(R6) J. T. Conway and L. D. Miller, "Detailed Analysis of the Phaze 1 Vertical Launch Seawolf Separation Unit Trials", British Aerospace Report BT 16964 (Confidential), Bristol, United Kingdom, September 1984.

(R5) L. D. Miller and J. T. Conway, "Preliminary Analysis of the Phaze 1 Vertical Launch Seawolf Separation Unit Trials at R.A.E. (Bedford)", British Aerospace Report BT 15822 (Confidential), Bristol, United Kingdom, December 1983.

(R4) J. T. Conway, "Vertical Launch Seawolf: Aero Information Note 15. User Guide for a Suite of Programs for Plotting Wind Tunnel Data for Vertical Launch Seawolf",
British Aerospace Report 255/JTC/VLSW/761, Bristol, United Kingdom, November 1983.

(R3) J. T. Conway, "Vertical Launch Seawolf: Aero Information Note 14. Piston Load Predictions For VLSW Separation Mechanism Cold Gas Tests", British Aerospace Report 255/JTC/VLSW/732, Bristol, United Kingdom, October 1983.

(R2) J. T. Conway, "Vertical Launch Seawolf: Aero Information Note 8. Induced Rolling Moments", British Aerospace Report 255/JTC/VLSW/538 (Confidential), Bristol, United Kingdom, February 1983.

(R1) J. T. Conway, "Vertical Launch Seawolf: Aero Information Note 6. Roll-Rate Behaviour during Turnover", British Aerospace Report 255/JTC/VLSW/503 (Company Confidential), Bristol, United Kingdom, January 1983.

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