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| 035 | ⊔ | ⊔ | ‡a(MiU)99187539727506381 |
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| 040 | ⊔ | ⊔ | ‡aTRAAL ‡beng ‡cTRAAL |
| 049 | ⊔ | ⊔ | ‡aMAIN |
| 086 | 0 | ⊔ | ‡aD 301.45/46-2:74-29 |
| 100 | 1 | ⊔ | ‡aNelson, Robert C., ‡d1942- ‡eauthor. |
| 245 | 1 | 0 | ‡aResponse of aircraft encountering aircraft wake turbulence / ‡cRobert C. Nelson. |
| 264 | ⊔ | 1 | ‡aWright-Patterson Air Force Base, Ohio : ‡bAir Force Flight Dynamics Laboratory, Air Force Systems Command, ‡c1974. |
| 300 | ⊔ | ⊔ | ‡axv, 125 pages : ‡billustrations ; ‡c28 cm. |
| 336 | ⊔ | ⊔ | ‡atext ‡btxt ‡2rdacontent |
| 337 | ⊔ | ⊔ | ‡aunmediated ‡bn ‡2rdamedia |
| 338 | ⊔ | ⊔ | ‡avolume ‡bnc ‡2rdacarrier |
| 490 | 0 | ⊔ | ‡aAir Force Flight Dynamics Laboratory (U.S.). Technical report ; ‡vAFFDL TR 74-29 |
| 500 | ⊔ | ⊔ | ‡a"June 1974." |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliograpic references (pages 115-119) |
| 520 | ⊔ | ⊔ | ‡aThe investigation deals with the dynamic behavior of an airplane encountering aircraft wake turbulence. A digital computer simulation was developed to study the response of an aircraft flying into a trailing vortex wake. The simulation includes the complete six degree of freedom equations of motion, a description of the vortex velocity field, unsteady aerodynamics, and pilot control input. The parameters included the penetration angle, separation distance, aircraft size, and pilot control input. Predicted vortex induced motions are presented for general aviation, business, and light jet transport type aircraft. |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aAerodynamics. |
| 650 | ⊔ | 0 | ‡aTurbulence. |
| 650 | ⊔ | 0 | ‡aWakes (Aerodynamics) |
| 710 | 2 | ⊔ | ‡aAir Force Flight Dynamics Laboratory (U.S.), ‡esponsor. |
| 730 | 0 | ⊔ | ‡aTechnical Report Archive & Image Library (TRAIL) |
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