Loading...
Please wait, while we are loading the content...
Similar Documents
Estimation of attainable leading-edge thrust for wings at subsonic and supersonic speeds
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Mack, R. J. Barger, R. L. Carlson, H. W. |
| Copyright Year | 1979 |
| Description | The factors which place limits on the theoretical leading edge thrust are identified. An empirical method for the estimation of attainable thrust is presented. The method is based on the use of simple sweep theory to permit a two dimensional analysis, the use of theoretical airfoil programs to define thrust dependence on local geometric characteristics, and the examination of experimental two dimensional airfoil data to define limitations imposed by local Mach numbers and Reynolds numbers. Comparisons of theoretical and experimental aerodynamic characteristics for a series of wing body configurations are examined. |
| File Size | 1765105 |
| Page Count | 62 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19800001866 |
| Archival Resource Key | ark:/13960/t8tb5x99b |
| Language | English |
| Publisher Date | 1979-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Subsonic Speed Wing Planforms Aerodynamic Coefficients Estimates Computer Programs Wings Supersonic Speed Sweep Effect Mathematical Models Aerodynamic Characteristics Prediction Analysis Techniques Leading Edges Thrust Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
