Abstract
To investigate some transonic design principles for an airplane with a wing of moderate aspect ratio a series of windtunnel models have been designed and tested at FFA.
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References
Atraghji, E., Sörensén, H.: Effects of Reynolds number on swept wing-body configurations with high lift devices at transonic speeds. ICAS 74-04, 1974.
Gustavsson, S.A.L.: A computer program for the prediction of aerodynamic characteristics of wing-body-tail combinations at subsonic and supersonic speeds. FFA AU-635 Part 2, 1972.
Gustavsson, S.A.L., Hedman, S.G.: An improved version of a collocation method for the prediction of aerodynamic characteristics of wing-body-tail combinations at subsonic speeds. FFA AU-812 (to be published).
Schmidt, W., Vanino, R.:The analysis of arbitrary wingbody combinations in transonic flow using a relaxation method. Paper presented at Symposium Transsonicum II, Göttingen Sept. 8–13, 1975.
Gustavs son, A.L., Mattsson, R.: Transonic wind tunnel test of the PT3 model, a supercritical wing on a simple body. FFA AU-1134 Part 1, 1974. (Also published in DGLR 74-102 and in Z. Flugwiss. 23 (1975) S. 257-262.)
Gustavsson, A.L.: Design and test of a wind tunnel model PT2 with a sonic-roof-top wing on a simple body. FFA AU-928 (to be published).
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© 1976 Springer-Verlag, Berlin/Heidelberg
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Gustavsson, A.L., Hedman, S.G. (1976). Design and Test of a Sonic Roof-Top Pressure Distribution Wing. In: Oswatitsch, K., Rues, D. (eds) Symposium Transsonicum II. International Union of Theoretical and Applied Mechanics. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-81005-3_30
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DOI: https://doi.org/10.1007/978-3-642-81005-3_30
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-81007-7
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