Loading...
Please wait, while we are loading the content...
Similar Documents
Supersonic aerodynamic characteristics of a lifting-body orbiter model with a blunted delta planform at mach 2.30 to 4.60
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Blair Jr., A. B. |
| Copyright Year | 1972 |
| Description | An investigation has been made in the Langley Unitary Plan wind tunnel to determine the aerodynamic characteristics of a lifting-body orbiter model with a blunted delta planform. The model was tested at Mach numbers from 2.30 to 4.60, at nominal angles of attack from -4 deg to 60 deg and angles of sideslip from -4 deg to 10 deg, and at a Reynolds number of 2.5 million per foot. |
| File Size | 54558836 |
| Page Count | 96 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19720023341 |
| Archival Resource Key | ark:/13960/t9b61bh72 |
| Language | English |
| Publisher Date | 1972-09-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Aerodynamic Configurations Supersonic Speed Lifting Bodies Bluff Bodies Wind Tunnel Models Aerodynamic Characteristics Manned Spacecraft Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
