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Aerodynamic characteristics of a monoplanar missile concept with bodies of circular and elliptical cross sections
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Graves, E. B. |
| Copyright Year | 1977 |
| Description | Experimental aerodynamic characteristics of a low-drag missile concept with a body of circular cross section were compared to one with a body of 3:1 elliptical cross section, the bodies having identical cross section area distributions. The concepts were of monowing design with constant wing span. Tail surfaces were located flush at the body base with plus or minus 30 deg dihedral. Wind tunnel tests were performed at Mach numbers from 0.5 to 4.63 and at angles of attack from about -5 deg to 28 deg. |
| File Size | 11801931 |
| Page Count | 187 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19780007056 |
| Archival Resource Key | ark:/13960/t2c87391x |
| Language | English |
| Publisher Date | 1977-12-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Ellipticity Missiles Circular Shells Wind Tunnel Tests Wing Span Angle of Attack Cross Sections Aerodynamic Characteristics Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
