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Reevaluation of compressible-flow preston tube calibrations
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Allen, J. M. |
| Copyright Year | 1977 |
| Description | Revised zero-pressure-gradient, adiabatic wall skin-friction-balance data covering a Mach number range from 1.6 to 4.6 led to a reevaluation of existing compressible flow Preston tube calibration equations. |
| File Size | 728084 |
| Page Count | 26 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19770011441 |
| Archival Resource Key | ark:/13960/t2j727m2d |
| Language | English |
| Publisher Date | 1977-02-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Heat Transfer Supersonic Flow Adiabatic Flow Speed Indicators Skin Friction Calibrating Pitot Tubes Compressible Flow Mach Number Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |