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Investigation of two pitot-static tubes at supersonic speeds
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1948 |
| Description | The results of tests at a Mach number of 1.94 of an ogives-nose cylindrical pitot-static tube and similar tests at Mach numbers of 1.93 and 1.62 of a service pitot-static tube to determine body static pressures and indicated Mach numbers are presented and discussed. The radial pressure distribution on the cylindrical bodies is compared with that calculated by an approximate theory. |
| File Size | 1070714 |
| Page Count | 26 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930085521 |
| Archival Resource Key | ark:/13960/t0ht6zp0j |
| Language | English |
| Publisher Date | 1948-11-19 |
| Access Restriction | Open |
| Subject Keyword | Bodies - Surface Conditions Instruments, Flight Research Equipment, Free-flight Flow, Supersonic 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 |