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Comparison of calculated and experimental load distributions on thin wings at high subsonic and sonic speeds
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1957 |
| Description | A method for calculating the aerodynamic loading on a wing in combination with a body is presented. Calculated results are compared with experimentally measured data for two wing-body configurations throughout a range of Mach number up to 1.0. The magnitude and the distribution of spanwise loading of the calculated data are generally in good agreement with the experimental data. |
| File Size | 1567204 |
| Page Count | 47 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930085012 |
| Archival Resource Key | ark:/13960/t12n9vb4d |
| Language | English |
| Publisher Date | 1957-01-01 |
| Access Restriction | Open |
| Subject Keyword | Wings, Complete - Theory Mach Number Effects - Complete Wings Wing-fuselage Combinations - Airplanes Wings, Complete - Sweep Loads, Aerodynamic - Wings Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |