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Experimental pressure distributions for a family of blunt bodies at mach numbers from 2.49 to 4.63 and angles of attack from 0 deg to 15 deg
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1969 |
| Description | Pressure distributions for blunt body wind tunnel models at supersonic speeds and angles of attack from 0 to 15 degrees |
| File Size | 4352126 |
| Page Count | 88 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19690025922 |
| Archival Resource Key | ark:/13960/t0vq7pk29 |
| Language | English |
| Publisher Date | 1969-08-01 |
| 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 |