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Heat transfer tests of an 0.006-scale thin skin space shuttle thermocouple model (41-0) in the langley research center variable density tunnel at m equals 8 (oh13)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Walstad, D. G. |
| Copyright Year | 1974 |
| Description | Orbiter entry heating distributions were obtained, and phase change paint data was correlated with thermocouple data during a program of heat transfer testing on a 0.006 scale space shuttle orbiter vehicle. The orbiter was tested at 0, 30, and 35 degrees angle of attack at Reynolds numbers of 1, 2, 3, 4, and 6 million per foot. Temperature data were obtained from a total of 57 thermocouples. |
| File Size | 10262523 |
| Page Count | 244 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740025208 |
| Archival Resource Key | ark:/13960/t8vb2x80q |
| Language | English |
| Publisher Date | 1974-08-01 |
| Access Restriction | Open |
| Subject Keyword | Space Vehicles Scale Models Thermocouples Thin Walls Reynolds Number Skin Structural Member Space Shuttle Orbiters Temperature Measurement Hypersonic Speed Wind Tunnel Tests Angle of Attack Heat Transfer Coefficients Graphs Charts Heat Transfer 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 |
