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| 008 | 210222s1974 ohua rb f000 0 eng d | ||
| 035 | ⊔ | ⊔ | ‡a(MiU)99187539726206381 |
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| 035 | ⊔ | ⊔ | ‡a(OCoLC)1238031997 |
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| 049 | ⊔ | ⊔ | ‡aMAIN |
| 086 | 0 | ⊔ | ‡aD 301.45/46-2:74-137 |
| 100 | 1 | ⊔ | ‡aWilliams, J. G.. ‡eauthor. |
| 245 | 1 | 0 | ‡aAnalysis/Theory of controlled configured structures / ‡cby J.G. Williams. |
| 264 | ⊔ | 1 | ‡aWright-Patterson Air Force Base, Ohio : ‡bAir Force Flight Dynamics Laboratory, Air Force Systems Command, ‡c1974. |
| 300 | ⊔ | ⊔ | ‡aviii, 98 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 74-137 |
| 500 | ⊔ | ⊔ | ‡a"Final report for period May 1974 - December1974." |
| 500 | ⊔ | ⊔ | ‡a"December 1974." |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliograpic references (page 65) |
| 520 | ⊔ | ⊔ | ‡aThe purpose of this program was to develop an analytical base and define the potential advantages for configuring aircraft wing structure to conform to predetermined displacements and twists when subjected to flight loads. An advanced fighter wing was selected as a baseline and several alternate internal structural arrangements were formulated for a comparison. All work was done using aluminum materials. Comparisons were made between the baseline and alternate designs after each optimized for strength utilizing identical allowable stresses. This study indicated that Controlled Configured Structure (ccs) does produce desirable wing twist under applied maneuver loading which show an advanatge over conventional structure by improving aerodynamic characteristics (lower drag and inboard CP shift). These characteristics were shown to be achievable with essentially no weight or cost penalty and no effective change in flutter speed. The potential of combining passive airload induced twist and camber was projected. (Author). |
| 536 | ⊔ | ⊔ | ‡aReport prepared by Vought Systems Division, LTV Aerospace Corporation, Dallas, Texas, under contract no. ‡bF33615-74-C-3088. |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aAerodynamic load. |
| 650 | ⊔ | 0 | ‡aJet fighter planes ‡xDesign and construction. |
| 650 | ⊔ | 0 | ‡aAirplanes ‡xWings ‡xDesign and construction. |
| 710 | 2 | ⊔ | ‡aAir Force Flight Dynamics Laboratory (U.S.), ‡esponsor. |
| 710 | 2 | ⊔ | ‡aLTV Aerospace Corporation, ‡esponsor. |
| 730 | 0 | ⊔ | ‡aTechnical Report Archive & Image Library (TRAIL) |
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