Summary
This paper presents the multi-disciplinary design code PrADO-Sup for supersonic commercial transport aircraft which is a strongly modified and extended version of PrADO, the Preliminary Aircraft Design and Optimization Code developed at the Institute of Aircraft Design and Structural Mechanics of the Technical University of Braunschweig. The modular structure of PrADO-Sup is shown and all topics within the iteration and optimization loops are addressed. Detailed information is given on the integration of an advanced aerodynamic model. Here the higher order panel code HISSS, developed by DASA-LM, was implemented to provide data for a wide range of both subsonic and supersonic onflow conditions.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Preview
Unable to display preview. Download preview PDF.
References
W. Heinze: Ein Beitrag zur quantitativen Analyse der technischen und wirtschaftlichen Auslegungesgrenzen verschiedener Flugzeugkonzepte für den Transport großer Nutzlasten, Dissertation, ZLR-Forschungsbericht 94–01, 1994.
L. Fornasier: HISSS-A Higher-Order Subsonic/Supersonic Singularity Method for Calculating Linearized Potential Flow, AIAA-Paper 84–1646, 1984.
M. Kaufman, V. Balabanov, S.L. Burgee, A.A. Giunta, B. Grossman, W.H. Mason, L.T. Watson, R.T. Haftka: Variable-Complexity Response Surface Approximations for Wing Structural Weight in HSCT Design, AIAA-Paper 96–0089, 1996.
M. Orlowski, U. Herrmann: Aerodynamic Optimization of Supersonic Transport Configurations, In: Proc. 20th. Congress of the International Council of Aeronautical Sciences, Sorrent, Italien, 8.-13.9.1996, pp. 924–930.
W. Schneider: Experimentelle Bestimmung von Flügel-Rumpf-Interferenzen im Machzahlbereich Ma=0,5 bis Ma=2,0, AVA-Bericht 66 A 31, 1966.
Jean Rech and Clive S. Leyman: A Case Study by Aerospatiale and British Aerospace on the Concorde, AIAA Professional Study Series, 1980.
Author information
Authors and Affiliations
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 1997 Friedr. Vieweg & Sohn Verlagsgesellschaft mbH, Braunschweig/Wiesbaden
About this chapter
Cite this chapter
Seubert, R. (1997). The Preliminary Aircraft Design and Optimization Program for Supersonic Commercial Transport Aircraft PrADO-Sup. In: Körner, H., Hilbig, R. (eds) New Results in Numerical and Experimental Fluid Mechanics. Notes on Numerical Fluid Mechanics (NNFM), vol 60. Vieweg+Teubner Verlag, Wiesbaden. https://doi.org/10.1007/978-3-322-86573-1_40
Download citation
DOI: https://doi.org/10.1007/978-3-322-86573-1_40
Publisher Name: Vieweg+Teubner Verlag, Wiesbaden
Print ISBN: 978-3-322-86575-5
Online ISBN: 978-3-322-86573-1
eBook Packages: Springer Book Archive