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Results of tests of a 0.010- and 0.015-scale models of space shuttle orbiter configurations 3 and 3a in the ames research center 3.5 foot hypersonic wind tunnel (oa23)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Cleary, J. W. Mellenthin, J. A. Milam, M. D. Dziubala, T. J. |
| Copyright Year | 1974 |
| Description | Longitudinal and lateral-directional stability and control characteristics were evaluated at Mach numbers of 5.3, 7.3 and 10.3 at angles of attack up to 50 degrees with Beta = 0 degrees and, for a few cases, Beta = 5 degrees. Component force data, fuselage base pressures and shadowgraph patterns were recorded. |
| File Size | 33634877 |
| Page Count | 764 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740027162 |
| Archival Resource Key | ark:/13960/t45q9pw9c |
| Language | English |
| Publisher Date | 1974-09-01 |
| Access Restriction | Open |
| Subject Keyword | Space Vehicles Hypersonic Speed Directional Stability Aerodynamic Configurations Scale Models Wind Tunnel Stability Tests Lateral Stability Hypersonic Wind Tunnels Shadowgraph Photography Angle of Attack Directional Control Space Shuttle Orbiters Longitudinal Stability 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 |
