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Effect of a rectangular simulated wing on the pressure-drag coefficient of various boat tails at mach numbers from 0.60 to 1.47
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1969 |
| Description | Wind tunnel tests on conical boattails, nacelles, and rectangular wings |
| File Size | 6907809 |
| Page Count | 61 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19690016947 |
| Archival Resource Key | ark:/13960/t3nw46s94 |
| Language | English |
| Publisher Date | 1969-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |