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Low-subsonic aerodynamic characteristics of a 60 deg swept delta wing space shuttle orbiter
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Freeman Jr., D. C. |
| Copyright Year | 1973 |
| Description | An investigation was conducted in the Langley low-turbulence pressure tunnel to determine Reynolds number effects on the low-subsonic areodynamic characteristics and longitudinal control effectiveness of a North American Rockwell phase B delta-wing orbiter concept designated 134D. The model was tested over a range of Reynolds numbers, based on body length, from 5.25 million to 29.4 million, at Mach numbers less than 0.35, at angles of attack from approximately -2 to 28, and at angles of sideslip of 0 and -6. |
| File Size | 9974711 |
| Page Count | 58 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19730018153 |
| Archival Resource Key | ark:/13960/t25b4w27w |
| Language | English |
| Publisher Date | 1973-07-01 |
| Access Restriction | Open |
| Subject Keyword | Space Vehicles Subsonic Speed Reynolds Number Delta Wings Wind Tunnel Models Angle of Attack Aerodynamic Characteristics Space Shuttle Orbiters Longitudinal Stability Sideslip 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 |
