Loading...
Please wait, while we are loading the content...
Similar Documents
Body-surface pressure data on two monoplane-wing missile configurations with elliptical cross sections at mach 2.50
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Lamb, M. Allen, J. M. Hernandez, G. |
| Copyright Year | 1983 |
| Description | Tabulated body surface pressure data for two monoplane-wing missile configurations are presented and analyzed. Body pressure data are presented for body-alone, body-tail, and body-wing-tail combinations. For the lost combination, data are presented for tail-fin deflection angles of 0 deg and 30 deg to simulate pitch, yaw, and roll control for both configurations. The data cover angles of attack from -5 deg to 25 deg and angles of roll from 0 deg to 90 deg at a Mach number of 2.50 and a Reynolds number of 6.56 x 1,000,000 per meter. Very consistent, systematic trends with angle of attack and angle of roll were observed in the data, and very good symmetry was found at a roll angle of 0 deg. Body pressures depended strongly on the local body cross-section shape, with very little dependence on the upstream shape. Undeflected fins had only a small influence on the pressures on the aft end of the body; however, tail-fin deflections caused large changes in the pressures. |
| File Size | 15121774 |
| Page Count | 157 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19830026636 |
| Archival Resource Key | ark:/13960/t1hj1c32g |
| Language | English |
| Publisher Date | 1983-09-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Body-wing and Tail Configurations Missile Configurations Angle of Attack Pressure Measurement Cross Sections Missile Bodies Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
