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Inverse transonic airfoil design including viscous interaction
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Carlson, L. A. |
| Copyright Year | 1976 |
| Description | A numerical technique was developed for the analysis of specified transonic airfoils or for the design of airfoils having a prescribed pressure distribution, including the effect of weak viscous interaction. The method uses the full potential equation, a stretched Cartesian coordinate system, and the Nash-MacDonald turbulent boundary layer method. Comparisons with experimental data for typical transonic airfoils show excellent agreement. An example shows the application of the method to design a thick aft-cambered airfoil, and the effects of viscous interaction on its performance are discussed. |
| File Size | 414229 |
| Page Count | 9 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19770003412 |
| Archival Resource Key | ark:/13960/t4rj97d98 |
| Language | English |
| Publisher Date | 1976-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Transonic Flow Numerical Analysis Fluid Dynamics Turbulent Boundary Layer Pressure Distribution Airfoils Aircraft Design Aerodynamic Characteristics Mach Number Viscous Flow Cartesian Coordinates Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
