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Viscous wing theory development. volume 2: grumwing computer program user's manual
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Chow, R. R. Ogilvie, P. L. |
| Copyright Year | 1986 |
| Description | This report is a user's manual which describes the operation of the computer program, GRUMWING. The program computes the viscous transonic flow over three-dimensional wings using a boundary layer type viscid-inviscid interaction approach. The inviscid solution is obtained by an approximate factorization (AFZ)method for the full potential equation. The boundary layer solution is based on integral entrainment methods. |
| File Size | 5613196 |
| Page Count | 115 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19870000611 |
| Archival Resource Key | ark:/13960/t7zm07b9b |
| Language | English |
| Publisher Date | 1986-10-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Three Dimensional Bodies Transonic Flow Wings Approximation Inviscid Flow Boundary Layer Equations User Manuals Computer Programs Viscous Flow Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |