Form Factor and Critical Mach Number Estimation for Finite Wings
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Timothy Takahashi | Brian J. German | Shane Donovan | Matthew J. Daskilewicz | Arvin Shajanian | Timothy T. Takahashi | M. Daskilewicz | Arvin Shajanian | Shane Donovan
[1] Timothy W. Simpson,et al. Design and Analysis of Computer Experiments in Multidisciplinary Design Optimization: A Review of How Far We Have Come - Or Not , 2008 .
[2] E. Torenbeek,et al. Synthesis of Subsonic Airplane Design , 1979 .
[4] Leland M. Nicolai. Fundamentals of Aircraft Design , 1984 .
[5] H. Schlichting. Boundary Layer Theory , 1955 .
[6] L. R. Miranda,et al. A generalized vortex lattice method for subsonic and supersonic flow applications , 1977 .
[7] Timothy T. Takahashi,et al. Zero Lift Drag and Drag Divergence Prediction for Finite Wings in Aircraft Conceptual Design , 2010 .
[8] M. D. McKay,et al. A comparison of three methods for selecting values of input variables in the analysis of output from a computer code , 2000 .
[9] J. Anderson,et al. Fundamentals of Aerodynamics , 1984 .
[10] Daniel P. Raymer,et al. Aircraft Design: A Conceptual Approach , 1989 .
[11] Joseph A. Schetz,et al. Full Configuration Drag Estimation , 2009 .
[12] R. C. Feagin,et al. Delta method, an empirical drag buildup technique , 1978 .
[13] Donald J Graham,et al. A systematic investigation of pressure distributions at high speeds over five representative NACA low-drag and conventional airfoil sections , 1945 .
[14] Thomas J. Santner,et al. The Design and Analysis of Computer Experiments , 2003, Springer Series in Statistics.
[15] Ira H. Abbott,et al. Summary of Airfoil Data , 1945 .