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High Performance Executive Transport Design Employing Twin Oblique Lifting Surfaces
Technical Paper
2001-01-3031
ISSN: 0148-7191, e-ISSN: 2688-3627
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English
Abstract
This paper presents a new Trans-Atlantic high performance executive transport suitability equipped to offer accommodation for 19 first class passengers. The unique feature of this conceptual design is application of Twin Oblique Lifting Surfaces or TOLS configuration. Minimum goals for the design included: similar maximum takeoff gross weight; satisfactory field performance; good stalling characteristics; and, competitive fuel burn qualities at high-transonic and low-supersonic speeds, i.e. M0.90–1.20, compared to contemporary M0.75–0.85 large and super-large business jets. The vehicle is to be powered by two medium by-pass derivative engines based on the BMW-Rolls Royce BR715 in an effort to maximize the likelihood of availability, ensure adequate en route performance efficiency and fulfillment of yet to be ratified Stage 4 noise compliance requirements.
Citation
Isikveren, A., "High Performance Executive Transport Design Employing Twin Oblique Lifting Surfaces," SAE Technical Paper 2001-01-3031, 2001, https://doi.org/10.4271/2001-01-3031.Also In
References
- Taylor, J. Munson, K. “History of Aviation” Crown Publishers Inc 1978
- Campbell J.P. Drake, H.M. “Investigation of Stability and Control Characteristics of an Airplane Model with Skewed Wing in the Langley Free-Flight Tunnel” 1945
- Jones, R.T. “New Design Goals and a New Shape for the SST” Astronautics and Aeronautics 10 12 December 1972
- Jones, R.T. Nisbet J.W. “Transonic Transport Wings – Oblique or Swept?” Astronautics and Aeronautics January 1974
- Olson E.C. Selberg, B.P. “Experimental Determination of Improved Aerodynamic Characteristics Utilising Biplane Wing Configurations” Journal of Aircraft 13 April 1976
- Rhodes, M.D. Selberg, B. “Dual Wing, Swept Forward Swept Rearward Wing, and Single Wing Design Optimisation For High Performance Business Airplanes” 1982
- Pfenninger, W. “Design Considerations of Large Subsonic Long Range Transport Airplanes with Low Drag Boundary Layer Suction,”
- Gundlach J.F., IV Naghshineh-Pour, A. Gern, F. Tetrault, P.-A. Ko, A. Schetz, A. Mason, W.H. Kapania, B. Grossman, B. Haftka R.T. June 1999
- Isikveren, A.T. ” Methodology for Conceptual Design and Optimisation of Transport Aircraft” 1998
- Kendall, E.R. “The Minimum Induced Drag, Longitudinal Trim and Static Longitudinal Stability of Two-Surface and Three-Surface Airplanes” 1984
- Obert. E. “Some Aspects of Aircraft Design and Aircraft Operation” Lecture Series Sweden 1996
- Durand, W.F. “Aerodynamic Theory” V January 1943
- November 1996
- Isikveren, A.T. ”Methodology for Conceptual Design and Optimisation of Transport Aircraft” September 1998
- Svoboda, C. “Turbofan Engine Database as a Preliminary Design Tool” Aircraft Design Journal 2000
- Whitford, R. “Design for Air Combat“
- Kroo, I. “The Aerodynamic Design of Oblique Wing Aircraft” AIAA Paper 86-2624 October 1986
- van der Velden, A.J.M Torenbeek, E. “Design of a Small Oblique-Wing Transport Aircraft” Journal of Aircraft 26 3 March 1989
- Isikveren, A.T. ”The PD340-2 19 Passenger Turbofan Regional Transport-Feasibility Study” 1998
- Mason, W.H. “Analytical Models for Technology Integration in Aircraft Design” 1990
- Jones, R.T. “The Oblique Wing – Aircraft Design for Transonic and Low Supersonic Speeds” Acta Astronautica 4 Pergammon Press 1977
- Torenbeek, E. ”Synthesis of Subsonic Airplane Design” Delft University Press 1988
- Raymer, D.P. ”Aircraft Design: A Conceptual Approach” AIAA Educational Series 1992
- Melin, T. “A Vortex-Lattice MATLAB Implementation for Linear Aerodynamic Wing Applications” December 2000
- Wauquiez, C. Rizzi, A. “PABLO – Potential Flow Around Airfoils with Boundary Layer coupled One-way” Royal Institute of Technology, Department of Aeronautics Sweden 1999
- Young, A.D. ”The Aerodynamic Characteristics of Flaps” 1953
- Linnell, R. “Weight Estimation Methods” July 1979
- Scott, P.W. Nguyen D. ”The Initial Weight Estimate” SAWE Paper No. 2327
- Torenbeek, E. “Development and Application of a Comprehensive, Design-sensitive Weight Prediction Method for Wing Structures of Transport Category Aircraft” October 1994
- Sewall, W.G. McGhee, R.J. Viken, J.K. Waggoner, E.G. Walker, B.S. Millard, B.F. “Wind tunnel results for a high-speed, natural laminar-flow airfoil designed for general aviation aircraft” NASA Langley Research Centre November 1985
- Jones, R.T. Nisbet J.W. “Aeroelastic Stability and Control of an Oblique Wing” The Aeronautical Journal of the Royal Aeronautical Society August 1986
- Weisshaar, T. Zeiler, T. “Dynamic Stability of Flexible Forward Swept Wing Aircraft” Journal of Aircraft December 1983
- Jobe, C.E. “Prediction of Aerodynamic Drag” July 1984
- Saltzman, E.J. Hicks, J.W. “In-Flight Lift-Drag Characteristics for a Forward-Swept Wing Aircraft (and Comparisons with Contemporary Aircraft)” NASA Technical Paper 3414 December 1994
- Abbott, I.H. Von Doenhoff, A.E. ”Theory of Wing Sections” 1959
- Clancy, L.J. ”Aerodynamics” Longman Scientific & Technical 1975
- Currey, N. ”Aircraft Landing Gear Design: Principles and Practises” AIAA 1988
- Gillette, W.B. ”Nacelle Installation Analysis for Subsonic Transport Aircraft” AIAA Paper 77-102
- Graham, A. Jones, R.T. Boltz, F. “An Experimental Investigation of Three Oblique Wing and Body Combination at Mach Numbers Between 0.6 and 1.4” April 1973
- McCormick, B.W. ”Aerodynamics, Aeronautics and Flight Mechanics” John Wiley & Sons 1979
- Nelms, W.P., Jr. “Applications of Oblique-Wing Technology – An Overview” AIAA Paper 76-943 September 1976
- Niu, M.C.Y. ”Airframe Structural Design” Conmilit Press Ltd 1989
- Roskam, J. Dr. ”Airplane Design” I–VII 1986
- Schippers, K.A. ”Cowl Design Methodology”
- Tipton, B.J. Dudley E.S. “The Preliminary Design Analysis of a Unique Semi-Tailless Aircraft Configuration” AIAA Paper 952053 1995