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1999 Conference Publication Intake design for a scramjet flight experimentBoyce, R. and Paull, A. (1999). Intake design for a scramjet flight experiment. 22nd International Symposium on Shock Waves, Imperial College, London, UK, 18-23 July, 1999. Southampton, UK: University of Southampton. |
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1999 Journal Article Performance study of a power law starbodySabean, JW, Lewis, MJ, Mee, D and Paull, A (1999). Performance study of a power law starbody. Journal of Spacecraft and Rockets, 36 (5), 646-652. doi: 10.2514/2.3496 |
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1998 Conference Publication Performance study of a power law star bodySabean, John W., Lewis, Mark J., Mee, David and Paull, Allan (1998). Performance study of a power law star body. 8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 1998, Norfolk, VA, April 27, 1998-April 30, 1998. American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.1998-1617 |
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1998 Conference Publication Supersonic combustion - A shock tunnel and vitiation-heated slowdown tunnel comparisonBoyce R.R., Wendt M., Paull A., Chinzei N., Stalker R.J. and Miyajima H. (1998). Supersonic combustion - A shock tunnel and vitiation-heated slowdown tunnel comparison. American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.1998-941 |
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1998 Journal Article Experiments on cruise propulsion with a hydrogen scramjetStalker R.J. and Paull A. (1998). Experiments on cruise propulsion with a hydrogen scramjet. Aeronautical Journal, 102 (1011), 37-43. |
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1998 Conference Publication A joint American-Australian university hypersonic research programLewis M.J. and Paull A. (1998). A joint American-Australian university hypersonic research program. Reston, Virigina: American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.1998-1551 |
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1998 Conference Publication Scramjet testing in the T4 impulse facilityPaull A. and Stalker R.J. (1998). Scramjet testing in the T4 impulse facility. 8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 1998, April 27, 1998-April 30, 1998. American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.1998-1533 |
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1998 Conference Publication Shock tunnel skin friction measurement in a supersonic combustorGoyne, C. P., Stalker, R. J. and Paull, A. (1998). Shock tunnel skin friction measurement in a supersonic combustor. Reston, Virigina: American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.1998-943 |
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1996 Conference Publication A shock tunnel investigation of scramjet performance with partially premixed combustionStalker, R.J., Morgan, R.G. and Paull, A. (1996). A shock tunnel investigation of scramjet performance with partially premixed combustion. Space Plane and Hypersonic Systems and Technology Conference, 1996, *, 18-22 November 1996. Reston, Virigina: American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.1996-4534 |
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1995 Journal Article A driver gas detection device for shock tunnelsPaull A. and King M.D. (1995). A driver gas detection device for shock tunnels. Shock Waves, 4 (5), 289-291. doi: 10.1007/BF01416041 |
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1995 Conference Publication A skin friction gauge for impulsive flowsGoyne C.P., Paull A. and Stalker R.J. (1995). A skin friction gauge for impulsive flows. 31st Joint Propulsion Conference and Exhibit, 1995, July 10, 1995-July 12, 1995. Reston, Virigina: American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.1995-3152 |
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1995 Journal Article Scramjet thrust measurement in a shock tunnelPaull A., Stalker R.J. and Mee D.J. (1995). Scramjet thrust measurement in a shock tunnel. Aeronautical Journal, 99 (984), 161-163. doi: 10.1017/s0001924000027147 |
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1995 Journal Article Experiments on supersonic combustion ramjet propulsion in a shock tunnelPaull A., Stalker R.J. and Mee D.J. (1995). Experiments on supersonic combustion ramjet propulsion in a shock tunnel. Journal of Fluid Mechanics, 296 (-1), 159-183. doi: 10.1017/S0022112095002096 |
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1994 Conference Publication Measurement of Scramjet Thrust in Shock TunnelsStalker, R. J., Simmons, J. M., Paull, A. and Mee, D. J. (1994). Measurement of Scramjet Thrust in Shock Tunnels. AIAA 18th Aerospace Ground Testing Conference, Colorado Springs, Colorado, USA, 20-23 June, 1994. American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.1994-2516 |
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1994 Journal Article Shock tunnel measurements of hypervelocity blunted cone dragPorter L.M., Paull A., Mee D.J. and Simmons J.M. (1994). Shock tunnel measurements of hypervelocity blunted cone drag. AIAA journal, 32 (12), 2476-2477. doi: 10.2514/3.12318 |
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1993 Conference Publication Thrust Measurements of a Complete Axisymmetric Scramjet in an Impulse FacilityPaull, A., Stalker, R. J. and Mee, D. J. (1993). Thrust Measurements of a Complete Axisymmetric Scramjet in an Impulse Facility. AIAA and DGLR, 5th International Aerospace Planes and Hypersonics Technologies Conference, Munich, Germany, 30 November - 3 December, 1993. American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.1993-5168 |
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1992 Journal Article Test flow disturbances in an expansion tubePaull A. and Stalker R.J. (1992). Test flow disturbances in an expansion tube. Journal of Fluid Mechanics, 245 (-1), 493-521. doi: 10.1017/S0022112092000569 |
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1992 Journal Article Skin-friction gauge for use in hypervelocity impulse facilitiesKelly G.M., Simmons J.M. and Paull A. (1992). Skin-friction gauge for use in hypervelocity impulse facilities. AIAA journal, 30 (3), 844-845. doi: 10.2514/3.10996 |
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1991 Journal Article The effect on an acoustic wave as it traverses an unsteady expansionPaull A. and Stalker R.J. (1991). The effect on an acoustic wave as it traverses an unsteady expansion. Physics of Fluids A, 3 (4), 717-719. doi: 10.1063/1.858079 |
