Loftin LK, Smith HA. 1949. Aerodynamic characteristics of 15 NACA air- foil sections at seven Reynolds numbers from 0.7 x 106 to 9.0 x 106. Washington (DC): National Advisory Committee for Aeronautics.LOFTIN, L.K. AND SMITH, H.A. 1949 Aerodynamic characteristics of 15 NACA airfoil ...
Semantic Scholar digital.library.unt.edu ufdc.ufl.edu 相似文献 引证文献A Study of Aerodynamics of Low Reynolds Number Flexible Airfoils The interaction between aerodynamics and structural flexibility in a low Reynolds number environment is of considerable interest to biological and micro air vehicles. ...
Erwin, J. R., Savage, M., and Emery, J. C., 1956, "Two-Dimensional Low- Speed Cascade Investigation of NACA Compressor Blade Sections Having a Systematic Variation in Mean-Line Loading," National Advisory Committee for Aeronautics, Washington, DC, Report No. NACA TN 3817....
.. “Laminar boundary layer on a circular cone in supersonic flow at a small angle of attack,” N.A.C.A., T.N. 2521, Oct. 1951.Moore F K 1951 Laminar boundary layer on a circular cone in supersonic flow at a small angle of attack Technical Note 252...
Proceedings of the ASME Fluids Engineering Division Summer Meeting 2016: FEDSM 2016, Washington, DC, USA, July 10-14, 2016, volume 1A. SymposiaFeero, M.A., Lavoie, P., Sullivan, P.E.: Time- and Phase-Averaged Boundary Layer Measurements on a Controlled NACA 0025 Airfoil. In: ASME 2016...
Erwin, J. R., Savage, M., and Emery, J. C., 1956, "Two-Dimensional Low- Speed Cascade Investigation of NACA Compressor Blade Sections Having a Systematic Variation in Mean-Line Loading," National Advisory Committee for Aeronautics, Washington, DC, Report No. NACA TN 3817....
Lee, H. and Kang, S., "Flow characteristics of transitional boundary layer on the NACA0012 airfoil in wakes," Proceedings of FEDSM'98, Washington, DC , June 21-25 1998.H.K. Lee and S.H Kang, Flow characteristics of transitional boundary layer on the NACA0012 airfoil in wakes, Pro- ...
A Correlation of Low-Speed, Airfoil-Section Stalling Characteristics with Reynolds Number and Airfoil Geometry; NACA Technical Note 3963; NACA Technical: Washington, DC, USA, 1957. Hassan, A. Predicted Aerodynamic Characteristics of a NACA 0015 Airfoil Having a 25% Integral Type Trailing Edge Flap...