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0022680733
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The Joined Wing: An Overview
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March
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WOLKOVITCH, J., The Joined Wing: An Overview, J. of Aircraft, Vol 23, pp. 161-178, March 1986.
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J. of Aircraft
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Wolkovitch, J.1
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4
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Aerospace America, Dec. 01
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Aerospace America, Dec. 01, pp 50.
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Towards Design of Unconventional High Aspect Ratio Joined- Wing Type Aircraft Configurations
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A 2020 Vision,April, London UK
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NANGIA, R.K., PALMER, M.E. & TILMANN, C.P.,.Towards Design of Unconventional High Aspect Ratio Joined- Wing Type Aircraft Configurations., RAeS Conference.A 2020 Vision., April 2002, London UK.
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(2002)
RAeS Conference
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Nangia, R.K.1
Palmer, M.E.2
Tilmann, C.P.3
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7
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28844454577
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Towards Design and Optimisation of Unconventional High Aspect Ratio Joined-Wing Type Aircraft Configurations
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June, Cambridge UK
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NANGIA, R.K., PALMER, M.E. & TILMANN, C.P.,.Towards Design and Optimisation of Unconventional High Aspect Ratio Joined-Wing Type Aircraft Configurations., CEAS Conference, June 2002, Cambridge UK.
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(2002)
CEAS Conference
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Nangia, R.K.1
Palmer, M.E.2
Tilmann, C.P.3
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8
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84880774369
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ICAS 2002-25R2, Toronto, Canada
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NANGIA, R.K., PALMER, M.E. & TILMANN, C.P.,.On Design of Unconventional High Aspect Ratio Joined-Wing Type Aircraft Configurations., ICAS 2002-25R2, Toronto, Canada.
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On Design of Unconventional High Aspect Ratio Joined-Wing Type Aircraft Configurations
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Nangia, R.K.1
Palmer, M.E.2
Tilmann, C.P.3
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9
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2942738205
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AIAA-2003-0605, Jan, Reno, USA
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NANGIA, R.K., PALMER, M.E. & TILMANN, C.P.,.Unconventional High Aspect Ratio Joined-Wing Aircraft with Aft- & Forward- Swept Wing-Tips, AIAA-2003-0605, Jan. 2003, Reno, USA.
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Unconventional High Aspect Ratio Joined-Wing Aircraft With Aft- & Forward- Swept Wing-Tips
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Nangia, R.K.1
Palmer, M.E.2
Tilmann, C.P.3
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10
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2942738205
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AIAA-2003-3925, June, Orlando, FL, USA
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NANGIA, R.K., PALMER, M.E. & TILMANN, C.P., Unconventional High AR Joined-Wing Aircraft incorporating Laminar Flow, AIAA-2003-3925, June 2003, Orlando, FL, USA
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Unconventional High AR Joined-Wing Aircraft Incorporating Laminar Flow
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Nangia, R.K.1
Palmer, M.E.2
Tilmann, C.P.3
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14
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20744451502
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CEAS European Forum, Bath, UK
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NANGIA, R. K. & GALPIN, S.A., Towards Design of High-Lift Krueger Flap Systems with Mach & Reynolds No. Effects for Conventional & Laminar Flow Wings, CEAS European Forum, Bath, UK, 1995.
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Towards Design of High-Lift Krueger Flap Systems With Mach & Reynolds No. Effects For Conventional & Laminar Flow Wings
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Nangia, R.K.1
Galpin, S.A.2
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20744431984
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AIAA- 2002-0709, January
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NANGIA, R.K., PALMER, M.E. & DOE, R.H., A Study of Supersonic Aircraft with Thin Wings of Low Sweep, AIAA- 2002-0709, January 2002.
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(2002)
A Study of Supersonic Aircraft With Thin Wings of Low Sweep
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Nangia, R.K.1
Palmer, M.E.2
Doe, R.H.3
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18
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84896332658
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RTO AVT Symposium, Loen, Norway, May 01
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NANGIA, R.K. & MILLER, A.S. Vortex Flow Dilemmas & Control on Wing Planforms for High Speeds, RTO AVT Symposium, Loen, Norway, May 01.
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Vortex Flow Dilemmas & Control On Wing Planforms For High Speeds
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Nangia, R.K.1
Miller, A.S.2
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22
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84896356465
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ICAS-96-6.10.3, September, Sorrento, Italy
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NANGIA, R.K., PALMER, M.E. & HODGES, J., Flow Separation Prediction on Inlets with Mach & Reynolds Number Effects in Subsonic Flight, ICAS-96-6.10.3, September 1996, Sorrento, Italy.
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Flow Separation Prediction On Inlets With Mach & Reynolds Number Effects In Subsonic Flight
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Nangia, R.K.1
Palmer, M.E.2
Hodges, J.3
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23
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84896321290
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Flow Separation Prediction on 3-D Inlets with Mach & Reynolds Number Effects in Subsonic Flight
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October, Bristol, UK
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NANGIA, R.K., PALMER, M.E. & MARTIN, P.G., Flow Separation Prediction on 3-D Inlets with Mach & Reynolds Number Effects in Subsonic Flight, RAeS - IMechE Conference Engine-Airframe integration, October 1996, Bristol, UK.
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(1996)
RAeS - IMechE Conference Engine-Airframe Integration
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Nangia, R.K.1
Palmer, M.E.2
Martin, P.G.3
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24
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84896364942
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Modelling of 3-D Aircraft Inlets at Zero Speed (& Low Speeds with Cross-wind) & Flow Separation Prediction
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November, London, UK
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NANGIA, R.K., PALMER, M.E. & HODGES, J., Modelling of 3-D Aircraft Inlets at Zero Speed (& Low Speeds with Cross-wind) & Flow Separation Prediction, RAeS - IMechE Conference Verification of Design Methods by Test & Analysis, November 1998, London, UK.
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(1998)
RAeS - IMechE Conference Verification of Design Methods By Test & Analysis
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Nangia, R.K.1
Palmer, M.E.2
Hodges, J.3
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25
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84896373295
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Addressing the'Zero Speed' & Low-Speed Aspects of 3-D Aircraft Intakes, Modelling With & Without Ground Effect, In Presence of Cross-wind & Lip-flow Separation Prediction
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March, Pau, France
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NANGIA, R.K., PALMER, M.E. & HODGES, J., Addressing the'Zero Speed' & Low-Speed Aspects of 3-D Aircraft Intakes, Modelling With & Without Ground Effect, In Presence of Cross-wind & Lip-flow Separation Prediction, CEAS 7th European Propulsion Forum Aspects of Engine/Airframe Integration, March 1999, Pau, France.
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(1999)
CEAS 7th European Propulsion Forum Aspects of Engine/Airframe Integration
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Nangia, R.K.1
Palmer, M.E.2
Hodges, J.3
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