Abstract
In the preceeding chapters on “Son of Concorde, a Technology Challenge” and “Aerodynamic Multipoint Design Challenge” it was explained, that a well balanced contribution of new technologies in all major disciplines is required for realisation of a new Supersonic Commercial Transport (SCT). One of these technologies - usually one of the most important for aircraft-is aerodynamics. Here, the required “pure” aerodynamic technologies are specified in more detail, according to our present knowledge. Increasing insight into the problems may change the balance of importance of the individual technologies and may require some more contributions. We must never confine our knowledge to the knowledge base of an expert at a given time, but must stay open for new insights.
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References
Courant, R., Friedrichs, K. O. Supersonic Flow and Shock Waves Applied mathematical sciences, 21, Springer Verlag, New York, Berlin, Heidelberg, 1948/ 1976
Courant, R., Hilbert, D. Methoden der mathematischen Physik II Springer, 1968
Jeffrey, A., Taniuti, T. Non-linear Wave Propagation with Applications to Physics and Magnetohydrodynamics Academic Press, New York and London, 1964
Mertens, J. Instationäre Strömungen von Gasen mit brennbaren Partikeln, Kapitel A2 Dissertation RWTH Aachen, 1983
Sauer, R. Nichtstationäre Probleme der Gasdynamik Springer, 1966
Heinz, C. Die Richtungs-und Verträglichkeitsbedingungen der Charakteristikentheorie Institutsbericht, Lehrstuhl für Mechanik, RWTH Aachen, 1970
Küchemann, D. The aerodynamic design of aircraft Pergamon Press, Oxford, 1978/ 1985
Jones, R. T. The Minimum Drag of Thin Wings at Supersonic Speed According to Kogan’s Theory Theoret. Comput. Fluid Dynamics (1989) 1: 97–103
Kogan, M. N. On Bodies of Minimum Drag in Supersonic Gas Flow Prikl. Mat. Mekh., vol. XXI, no. 2, 1957, 207–212
Mann, M. J., Carlson, H. W. Aerodynamic Design of Supersonic Cruise Wings with a Calibrated Linearized Theory-Journal of Aircraft, 31, 1, Jan.-Feb. 1994, pp. 35–40
Van der Velden, A. Aerodynamic Design and Synthesis of the Oblique Flying Wing Supersonic Transport PhD-thesis Stanford University, Dept. Aero Astro SUDDAR 621, Univ. Microfilms no. DA9234183, June 1992
Engler, R. H., Hartmann, K., Schulze, B. Aerodynamic Assessment of an Optical Pressure Measurement System (OPMS) by Comparison with Conventional Pressure Measurements in a High Speed Wind Tunnel Paper, presented at ICIASF ‘81, Washington D.D., 8 pages
Vollan, A., Mati, L. A new Optical Pressure Measurement System Paper, presented at ICIASF ‘81, Washington D. C., 7 pages
McLachlan, B. G., Bell, J. H., Park, H., Kennelly, R. A., Schreiner, J. A., Smith, S.C. Strong, J. M. Pressure-Sensitive Paint Measurements on a Supersonic High-Sweep Oblique Wing Model Journal of Aircraft, 32, 2, March-April 1995, 217–227
Willert, C. E. A Comparison of Several Particle Image Velocimetry Systems DGLR-Bericht 94–04 “Strömungen mit Ablösung”, Erlangen, 4.-7. 10. 1994, 266–271
Lienhart, H., Böhnert, T. Grenzschichtmessungen an einem Laminarflügelprofil mit einem Laser-Doppler-Anemometer DGLR-Bericht 92–07 “Strömungen mit Ablösung”, Köln-Porz, 10.-12. 11. 1992, 471–476
Barreau, R., Renard, T. (Reporters) BRITE EURAM Program “Supersonic Flow Phenomena”, Final Report Subtask 1.3 “Preliminary Aeroelastic Investigation of Supersonic Transport Aircraft Configuration”
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© 1997 Springer-Verlag Wien
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Mertens, J. (1997). Required Aerodynamic Technologies. In: Sobieczky, H. (eds) New Design Concepts for High Speed Air Transport. International Centre for Mechanical Sciences, vol 366. Springer, Vienna. https://doi.org/10.1007/978-3-7091-2658-5_5
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DOI: https://doi.org/10.1007/978-3-7091-2658-5_5
Publisher Name: Springer, Vienna
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