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Reynolds number and mach number effect on space shuttle configurations
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Zakkay, V. |
| Copyright Year | 1973 |
| Description | Analytical studies have been conducted concerning the lee-surface flow phenomena over a space shuttle orbiter model based on the experimental data obtained during September, 1971 through August, 1972. Lee-surface peak heating phenomena and flow separation patterns were analyzed. Major results of analyses are briefly presented. |
| File Size | 1456113 |
| Page Count | 23 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740004381 |
| Archival Resource Key | ark:/13960/t6k11v976 |
| Language | English |
| Publisher Date | 1973-08-31 |
| Access Restriction | Open |
| Subject Keyword | Space Vehicles Boundary Layer Separation Separated Flow Space Shuttle Orbiters Heat Transfer Reynolds Number Mach Number 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 |