A study of supersonic aircraft with thin wings of low sweep

40th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2002, Pages

  Nangia, R K ^a   Palmer, M E ^a   Doe, R H ^a  

^a Nangia Aero Research Associates   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 84894340523     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (14)

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2. KROO, I. et al, "Supersonic Laminar Technology", DARPA www. April 2000.
3. WARWICK, G., "Supersonic and Silent", Flight International, Vol. 158, No.4746, 12-18 September 2000.
4. KUCHEMANN, D. "The Aerodynamic Design of Aircraft", Pergamon.
5. NANGIA, R.K., "Low Speed Performance Optimisation of Advanced Supersonic Civil Transport with Different LE & TE Devices", EAC'94, Toulouse, France, Ocl94.
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7. NANGIA, R.K., "Development of an Inverse Design Technique using 3-D Membrane Analogy", Future Paper.
8. NANGIA, R.K. & GALPIN, S.A., "Towards Design of High-Lift Knieger Flap Systems with Mach & Reynolds No. Effects for Conventional & Laminar Flow Wings". CEAS European Forum, Bath, UK, 1995.
9. NANGIA, R. K. & GALPIN, S.A., "Prediction of LE & TE Devices Aerodynamics in Hish-Lift Configurations with Mach & Reynolds No. Effects", ICAS-1996-12.7.6.
10. NANGIA, R.K. & GREENWELL. D.I. "Wins Design of an Oblique-Wing Combat Aircraft", ICAS-2000-1.6.1.
11. NANGIA, R.K., PALMER, M.E. & GREENWELL. D.I., "Design of Conventional & Unconventional Wings for UAV's", RTO-AVT Symposium, "Advanced Flow Management, Vortex Rows & High Angle of Attack", Turkey, October 2000
12. GRANTZ, A.C., "Leading Edge Flap Planform Effects for Wings of Moderate Leading Edge Sweep". AIAA-85-5005, 1985.
13. HARVEY, W.D. & FORMAN, B., "Future Regional Aircraft Market Constraints".
14. FUHRMANN, H.D. "Application of NLF to a Supersonic Transport Concept", AIAA 93-3467, Aug. 1993.