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Flexstab analysis
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Lowder Jr., H. E. |
| Copyright Year | 1976 |
| Description | The wing differential pressure distributions of two vehicles are predicted using FLEXSTAB. Three space shuttle configurations were investigated. Comparisons were made of wind tunnel and analytical data for a selected range of angle of attack, angle of sideslip, and Mach number. A drone-type vehicle was investigated and comparisons were made between flight and analytical data of wing pressure distributions and static longitudinal stability derivatives. |
| File Size | 4186597 |
| Page Count | 13 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19760011965 |
| Archival Resource Key | ark:/13960/t0ht7dm4b |
| Language | English |
| Publisher Date | 1976-02-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Wings Space Shuttles Wind Tunnel Tests Pressure Distribution Aerodynamic Stability Prediction Analysis Techniques Stability Derivatives Computer Programs Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |