Program is revised of NASA/Lockheed program to numerically analyze complex viscous flow about slotted airfoils. Airfoil to be analyzed can contain as many as 10 components with negative or positive overlap. Program is written in FORTRAN IV and Assembled for batch execution on CYBER 175 only.
Improved multielement airfoil analysis
NASA Tech Briefs ; 5 , 1
1980-08-01
Miscellaneous
No indication
English
Multielement airfoil ice accretion
AIAA | 1995
|Multipoint Inverse Method for Multielement Airfoil Design
Online Contents | 1998
|