Publikationsdatum:
2019-07-13
Beschreibung:
A new inverse airfoil design method has been developed. This method couples a two-dimensional Navier-Stokes code to a residual-correction design algorithm to produce an efficient design code. Since this method can be used to design airfoils near the limits of performance capabilities, a technique to investigate the limits of lift has been developed to guide the design of new airfoils. Examples of the use of the inverse Navier-Stokes code and the maximum lift technology in the design of new airfoils are presented.
Schlagwort(e):
AERODYNAMICS
Materialart:
AHS, Annual Forum; May 21, 1990 - May 23, 1990; Washington, DC; United States
Format:
text
Permalink