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Supersonic aerodynamic characteristics of a tail-control cruciform maneuverable missile with and without wings
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Spearman, M. L. |
| Copyright Year | 1983 |
| Description | The aerodynamic characteristics for a winged and wingless cruciform missile configuration were examined. The configuration had an ogive-cylinder body with a 3.5 caliber forebody; an overall length-to-diameter ratio of 11.667; and had cruciform tails that were trapezoidal in planform. Tests were made both with and without 72.9 degree cruciform delta wings. The investigation was made for Mach numbers from 1.50 to 4.63, roll attitudes of 0 degrees and 45 degrees, angles of attack from -4 degrees to 22 degrees, and tail control deflections from 10 degrees to -40 degrees. |
| File Size | 481555 |
| Page Count | 12 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19830009235 |
| Archival Resource Key | ark:/13960/t49p7w57m |
| Language | English |
| Publisher Date | 1983-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Cruciform Wings Missile Configurations Trapezoidal Wings Supersonic Flight Delta Wings Ogives Angle of Attack 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 |
