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A two-dimensional, iterative solution for the jet flap
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Herold, A. C. |
| Copyright Year | 1973 |
| Description | A solution is presented for the jet-flapped wing in two dimensions. The main flow is assumed to be inviscid and incompressible. The flow inside the jet is considered irrotational and the upper and lower boundaries between the jet and free stream are assumed to behave as vortex sheets which allow no mixing. The solution is found to be in satisfactory agreement with two dimensional experimental results and other theoretical work for intermediate values of momentum coefficient, but the regions of agreement vary with jet exit angle. At small values of momentum coefficient, the trajectory for the jet, as computed by this method, has more penetration than that of other available data, while at high values of moment coefficient this solution results in less penetration of the jet into the main flow. |
| File Size | 1862377 |
| Page Count | 49 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19730007259 |
| Archival Resource Key | ark:/13960/t51g5g21c |
| Language | English |
| Publisher Date | 1973-02-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Numerical Analysis Aerodynamic Configurations Jet Flaps Two Dimensional Flow Wing Slots Aerodynamic Characteristics Lift Augmentation Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
