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Effects of configuration modifications on aerodynamic characteristics of tension shell shapes at mach 3.0
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1967 |
| Description | Configuration modifications of tension shell shapes to improve aerodynamic characteristics at Mach 3 by delaying onset of flow separation |
| File Size | 8739536 |
| Page Count | 39 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19670024666 |
| Archival Resource Key | ark:/13960/t6j14sp36 |
| Language | English |
| Publisher Date | 1967-08-01 |
| Access Restriction | Open |
| Subject Keyword | Shell Stability Flow Separation Aerodynamic Characteristics 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 |