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| 040 | ⊔ | ⊔ | ‡aTRAAL ‡cTRAAL |
| 049 | ⊔ | ⊔ | ‡aMAIN |
| 086 | 0 | ⊔ | ‡aD 217.22:72-80 |
| 100 | 1 | ⊔ | ‡aTetervin, Neal, ‡eauthor. |
| 245 | 1 | 0 | ‡aCalculation of magnus forces on axisymmetric bodies at small angles of attack with incompressible turbulent boundary layers / ‡cprepared by Neal Tetervin. |
| 264 | ⊔ | 1 | ‡aWhite Oak, Maryland : ‡bUnited States Naval Ordnance Laboratory, ‡c1972. |
| 300 | ⊔ | ⊔ | ‡axii, 59 [88] pages ; ‡billustrations ; ‡c28 cm. |
| 336 | ⊔ | ⊔ | ‡atext ‡btxt ‡2rdacontent |
| 337 | ⊔ | ⊔ | ‡aunmediated ‡bn ‡2rdamedia |
| 338 | ⊔ | ⊔ | ‡avolume ‡bnc ‡2rdacarrier |
| 490 | 0 | ⊔ | ‡aNOLTR (Series) ; ‡v72-80 |
| 500 | ⊔ | ⊔ | ‡a"12 March 1972". |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references (pages 58-59) |
| 520 | ⊔ | ⊔ | ‡aThe Magnus force is found by adding the boundary layer displacement surface to the body and then calculating the force on the resulting non- axisymmetric body. The displacement surface is calculated by the simultaneous integration of a differential equation for a streamline, two partial-differential boundary layer integral-momentum equations with the boundary layer thickness and the tangent of the angle between the local direction of the surface friction and potential flow streamline as dependent variables, and a partial differential equation for the displacement surface thickness. The method is applied to a half-ellipsoid of fineness ratio 5 at 4 degrees angle of attack. Slender-body theory is used to calculate the force. |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aTurbulent boundary layer. |
| 650 | ⊔ | 0 | ‡aAngle of attack (Aerodynamics) |
| 650 | ⊔ | 0 | ‡aMagnus effect. |
| 710 | 2 | ⊔ | ‡aNaval Ordnance Laboratory (White Oak, Md.) |
| 730 | 0 | ⊔ | ‡aTechnical Report Archive & Image Library (TRAIL) |
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