Aerodynamic tradeoff study of conventional, canard, and trisurface aircraft systems
- 1 October 1986
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 23 (10) , 768-774
- https://doi.org/10.2514/3.45379
Abstract
No abstract availableKeywords
This publication has 11 references indexed in Scilit:
- Analytical Study of Three-Surface Lifting SystemsPublished by SAE International ,1985
- The minimum induced drag, longitudinal trim and static longitudinal stability of two-surface and three-surface airplanesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Aerodynamic design optimization trim analysis of canard conventionalconfigurationsJournal of Aircraft, 1984
- Aerodynamic optimization, comparison, and trim design of canard and conventional high performance general aviation configurationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Minimum Induced Drag of Canard ConfigurationsJournal of Aircraft, 1982
- Effect of downwash on the induced drag of canard-wing combinationsJournal of Aircraft, 1982
- Aerodynamic Design Data For a Cruise-Matched High Performance Single Engine AirplaneSAE International Journal of Advances and Current Practices in Mobility, 1981
- Prandtl's biplane theory applied to canard and tandem aircraftJournal of Aircraft, 1980
- Calculation of profile drag of airfoils at low Mach numbers.Journal of Aircraft, 1968
- Approximate Calculation of the Laminar Boundary LayerAeronautical Quarterly, 1949