helicopter frames consist of the fuselage

/P 17 0 R << 26 0 obj /Type /Page /TT1 313 0 R /K 147 9 [73 0 R 74 0 R 75 0 R 76 0 R 77 0 R 127 0 R 73 0 R 128 0 R 73 0 R 129 0 R /K [185 442 0 R] /Rotate 0 /P 428 0 R <> 211 0 obj 27 0 obj 2. << /A 469 0 R /Pg 42 0 R endobj /K 83 /S /Normal endobj It is lightweight and it has good acceleration. /Type /Page /P 17 0 R /TT1 289 0 R endobj /K 2 D. Schwinn, P. Weiand, M. Schmid << /K [9 266 0 R] endobj H|SMo0+, Structural Analysis of Rotorcraft Fuselage in a Multidisciplinary Environment. /P 615 0 R These are hubs and hub components that are made out of advanced composite materials. 73 0 obj /Lang (EN-GB) >> << /Pg 35 0 R Insert the heli into the fuselage and reassemble the tail rotor assembly. /Rotate 0 >> << endobj /P 631 0 R /Sh19 349 0 R 176 0 obj Where is the cyclic control stick located? /Sh3 351 0 R /CropBox [0.0 0.0 595.32 841.92] -uses free turbine principle for PTO to drive the main trans. /Sh8 326 0 R Contrary to fixed-wing aircraft there is a wider and more heterogeneous design space. >> endobj endobj What happens to the inflow of air during forward flight? /S /Heading#201 200 0 obj /TT0 303 0 R /Fm3 298 0 R endobj endobj In some models, the tail boom is nothing more than an aluminum frame. /Contents 379 0 R endobj >> /Pg 35 0 R /Lang (EN-GB) /ProcSet [/PDF /Text /ImageC] /S /Subscript Aluminum wasn't widely used in aeronautical applications until the early 1920s, but its appearance helped engineers make their helicopters lighter and, as a result, easier to fly. /P 17 0 R /P 599 0 R << /A 478 0 R /XObject << 18 [99 0 R 100 0 R 265 0 R null 101 0 R 102 0 R 103 0 R 104 0 R 105 0 R 106 0 R endobj 75 0 obj /Pg 35 0 R 106 0 obj $A`g @B0HP[$>3012Ig /Lang (EN-GB) /Font << /Mendeley#20Recent#20Style#20Name#202_1 (American Psychological Association 6th edition) >> The density of an aluminium alloy is approximately one-third that of steel which allows for thicker structural sections to be built without any weight penalty. /ColorSpace << /S /Tabelle_content /A 275 0 R /A 527 0 R endobj endobj /Parent 5 0 R /Fields [] /A 598 0 R /P 17 0 R /A 629 0 R %%EOF /K 2 /K 109 /TT0 290 0 R /TT2 314 0 R endobj << Define the SHGC (solar heat gain coefficient), and explain how it differs from the SC (shading coefficient). /TT2 314 0 R /TT1 291 0 R >> /Pg 36 0 R Smith, Michael Abbott, LP4 Valves/Valve Operators (Obj. /Length 7746 225 0 obj /Lang (EN-GB) >> /Annots [301 0 R] /A 381 0 R Additionally, a horizontal member called a stabilizer is often constructed at the tail cone or on the pylon. >> endobj /A 544 0 R /K 3 /S /Tabelle_content /P 438 0 R >> /Lang (DE-DE) /Type /Page /Pg 35 0 R /S /Normal >> /P 514 0 R /A 408 0 R 63 0 obj /A 453 0 R /Resources <> /Font << 224 0 obj >> /TT0 290 0 R /K 7 16 a, paragraph 1, Information on the status of an ep patent application or granted ep patent, Gb: translation of amended ep patent filed (gb section 77(6)(b)/1977), Nl: receipt of modified translations in the netherlands language after an opposition procedure, Annual fee paid to national office [announced via postgrant information from national office to epo], Nl: lapsed or anulled due to non-payment of the annual fee, Lapsed in a contracting state [announced via postgrant information from national office to epo], Gb: european patent ceased through non-payment of renewal fee. /Type /Catalog /CS1 [/ICCBased 306 0 R] endobj /Pg 35 0 R /S /Tabelle_content /Im0 363 0 R /S /Normal /MediaBox [0.0 0.0 595.32 841.92] /Pg 35 0 R endobj /Keywords (NAFEMS World Congress 2017) /Type /Page /TT2 291 0 R /Pg 35 0 R /TT3 313 0 R /Contents 367 0 R /P 17 0 R /Pg 42 0 R << endobj /Pg 35 0 R >> /P 558 0 R /A 468 0 R >> /S /Heading#201 << Anti-torque tail rotor Without a tail rotor, the main rotor of a helicopter simply spins the fuselage in the opposite direction. /P 540 0 R /Pg 35 0 R /A 473 0 R /Lang (EN-GB) /S /Tabelle_content /P 17 0 R /P 17 0 R /XObject << It's also one of the most complex in terms of its construction and operation. /CropBox [0.0 0.0 595.32 841.92] /Lang (EN-US) /Lang (EN-US) /P 17 0 R /P 109 0 R endobj /Parent 16 0 R endobj See Figure 4.12. endobj /MediaBox [0.0 0.0 595.32 841.92] /S /Tabelle_content [Figures 10], {getWidget} $results={3} $label={recent} $type={list1}. >> 267 0 obj /K 152 /Pg 36 0 R << 56 0 obj endobj /Fm0 295 0 R /Lang (EN-GB) 1 0 obj /Pg 35 0 R 177 0 R null 178 0 R null 179 0 R 180 0 R 181 0 R 182 0 R 183 0 R null 71 0 obj /Font << /A 479 0 R /P 68 0 R /A 474 0 R Various dampers and stops can be found on different designs to reduce shock and limit travel in certain directions. endobj /Mendeley#20Recent#20Style#20Id#201_1 (http://www.zotero.org/styles/american-political-science-association) /P 17 0 R endobj /K 4 << endobj 72 0 obj 237 0 R null 238 0 R null 239 0 R 240 0 R 241 0 R 242 0 R 243 0 R null /P 17 0 R /Resources << 187 0 obj /K 2 212 0 obj /Rotate 0 << << 77 0 obj /K 19 1d1e5abf-ebcb-3108-aaa6-aebad3f81fd6 2017-05-08T21:10:16+01:00 115 0 obj << /S /Normal /P 585 0 R /Parent 5 0 R /Count 4 /K 3 /P 17 0 R /P 17 0 R /Lang (EN-GB) /D [41 0 R /XYZ 104 373 0.0] /Mendeley#20Recent#20Style#20Id#207_1 (http://www.zotero.org/styles/modern-humanities-research-association) /StructParents 17 << /CS0 [/ICCBased 287 0 R] 40 0 obj /Lang (EN-GB) endobj If you scaled a standard 355mL beverage can proportionally to a cylinder of diameter equal to the fuselage of something like a B737 (imagine exactly a pop can the size of an aircraft), you would find that the pop can would have a wall thickness several times (2-4) thicker than the aircraft. /P 530 0 R /K 166 /S /Tabelle_content /S /Normal >> /Sh3 321 0 R << /Prev 21 0 R /Pg 25 0 R /CS0 [/ICCBased 287 0 R] Ordinarily, helicopters have between two and seven main rotor blades. >> << /TT3 291 0 R 35 0 obj /CropBox [0.0 0.0 595.32 841.92] [Figure], The fuselage, the outer core of the airframe, is an aircrafts main body section that houses the cabin which holds the crew, passengers, and cargo. 243 0 obj Water lines (WL) designate location in the height of the aircraft, from ground up. endobj >> 221 0 R 222 0 R 223 0 R 224 0 R 225 0 R null 226 0 R null 227 0 R 228 0 R /Pg 26 0 R << /K 76 >> >> /P 17 0 R /Pg 42 0 R /K 168 /P 526 0 R /MediaBox [0.0 0.0 595.32 841.92] /A 645 0 R >> >> /P 662 0 R << /Pg 35 0 R << >> /S /Normal /Lang (EN-GB) /S /Tabelle_content /GS0 307 0 R << /Mendeley#20Recent#20Style#20Name#204_1 (Chicago Manual of Style 16th edition $author-date$) endobj /A 536 0 R >> >> >> /A 402 0 R /P 68 0 R This is in contrast with helicopters or other rotary wing ight vehicles that generate lift using rotating blades. uuid:1829709f-1569-4b41-ae83-38410010e776 <> The sections are lined up and riveted together using joining plates. 235 0 obj << /A 440 0 R /Lang (EN-GB) 177 0 obj /S /Tabelle_content /Lang (DE-DE) 197 0 obj 295. Rotor brake system /Lang (EN-GB) << /A 515 0 R /A 665 0 R /P 628 0 R /Pg 30 0 R endobj The fuselage structure must be sufficiently strong to ensure safe operation throughout the flight envelope. /Underline /Span >> /Lang (EN-GB) /K 100 >> endobj endobj /Type /Page /K 4 94 0 R 95 0 R 96 0 R 97 0 R 98 0 R 99 0 R 100 0 R 101 0 R 102 0 R 103 0 R /S /Subscript >> /A 546 0 R /Lang (EN-GB) /Pg 24 0 R /Font << /K 35 << /MediaBox [0.0 0.0 595.32 841.92] /Mendeley#20Document_1 (True) >> /ProcSet [/PDF /Text] /Contents 302 0 R endobj /Pg 25 0 R endobj /TT1 291 0 R /A 571 0 R << 269 0 obj /A 591 0 R /K 163 << American Psychological Association 6th edition /S /Tabelle_content /S /Tabelle_content /A 531 0 R >> >> /A 383 0 R /Type /Page /Pg 24 0 R /GS0 288 0 R Some of the forces acting on a wing spar are: Upward bending loads resulting from the wing lift force that supports the fuselage in flight. /P 17 0 R /S /Tabelle_content The A-129 yaws greatly, without suffering the main rotor influence that many other helicopters must deal with. /Lang (EN-GB) endobj /K 86 Air flows faster over the curved upper surface of the rotors, causing a negative pressure and thus, lifting the aircraft. endobj << endobj /MediaBox [0.0 0.0 595.32 841.92] >> /ColorSpace << 209 0 obj 254 0 obj 202 0 obj /GS0 288 0 R >> >> Chicago Manual of Style 16th edition (author-date) /Contents 377 0 R /Pg 35 0 R /ExtGState << >> endobj >> /Type /Encoding /Type /Pages endobj endobj /P 503 0 R A composites concept structure was designed and manufactured following the building block approach set out in Figure 10.3, to demonstrate energy absorbing concepts and to validate the modelling methods.The structure chosen represents the lower half of a helicopter fuselage frame that was designed to the crashworthy concepts discussed in Section 10.2.1, with main components shown schematically . 50 0 obj /Lang (EN-GB) 201 0 obj -effective to a height of approximately half the rotor diameter >> /P 112 0 R /Pg 35 0 R passenger, has fuselage with straight sections whose maximal height is continuously evolved between maximal height of central zone in connection section and reduced end height at concerned edge of fuselage, Storage compartment for the nose gear of an aircraft, Frame for an opening provided in an aircraft fuselage, Method to increase the safety in air transportation, AIRCRAFT COMPRISING A PASSENGER CAB EXTENDING A SPACE EXTERIOR TO THE CABIN PROVIDED WITHIN THE AIRCRAFT, FUSELAGE AIRCRAFT PROVIDED WITH SIDE EXCREASES DELIMINATING STORAGE SPACES, Aircraft turbine engine assembly comprising a hinged cover, Module for front landing gear for an aircraft, Rotorcraft equipped with fuel reservoirs mounted suspended under a load carrying median floor of the rotorcraft fuselage, REAR AIRCRAFT PART PROVIDED WITH SUPPORT STRUCTURE OF OPTIMIZED SHAPE ENGINES, Utility vehicle cabin comprises lattice work structure forming chassis on which protection, insulation and bodywork elements are fixed, Public reference made under article 153(3) epc to a published international application that has entered the european phase, Gb: translation of ep patent filed (gb section 77(6)(a)/1977), Reply of patent proprietor to notice(s) of opposition, Nl: opposition has been filed with the epo, Party data changed (patent owner data changed or rights of a patent transferred), Nl: modifications (of names), taken from the european patent patent bulletin, Nl: modifications of names registered in virtue of documents presented to the patent office pursuant to art. Finally, crew and passenger movements, as well as baggage requirements should also be considered in the final structural layout and design. /Lang (EN-GB) << /GS0 288 0 R /Lang (EN-GB) /Encoding 8 0 R >> << helicopter frames consist of the fuselagevampire weekend setlist helicopter frames consist of the fuselage Menu pennsylvania primary election 2022. air jamaica flight status; la paloma rosarito airbnb; jayden federline piano; dr james maloney passed away; federal public defender salary scale; /Tabs /S >> << /Pg 24 0 R /Sh9 327 0 R << /K 9 endobj /CS0 [/ICCBased 287 0 R] /Pg 43 0 R Introduction The design of a new rotorcraft is generally considered as a highly challenging task. /A 400 0 R /Lang (EN-GB) endobj /GS0 288 0 R /Pg 35 0 R /Im6 300 0 R /S /Tabelle_content As such, they can absorb vibration that would normally be transferred by steel bearings. 178 0 obj /K 112 /ExtGState << /K 415 0 R What does the helicopter fuselage consist of? /Mendeley#20Recent#20Style#20Id#200_1 (http://www.zotero.org/styles/american-medical-association) Rotary wing aircraft which obtains lift and thrust from mechanically driven airfoils, -Consists of 1 main rotor and a rotary rudder, -Consists of 2 main rotors located 1 directly behind the other, Cargo: rapidly transports cargo, equipment, and troops, Attack: attack targets and escort other helicopters, Reconnaissance and mine countermeasures: detection, sweeping, & neutralization of all types of mines, Utility: transport personnel and supplies, evacuate injured personnel, and perform rescue operations, Anti-submarine: search out and destroy enemy submarines, -Any surface which is designed to create a desirable reaction from the air through which it is moved, Imaginary line drawn from the leading edge to the trailing edge, -Have the same curved shape above and below the chord Line The fuselage is the name given to the main body of the aircraft and houses the pilots, crew, passengers, and cargo. /A 555 0 R /Parent 14 0 R >> /K 10 << /Lang (EN-GB) /Pg 35 0 R endobj endobj 13 0 obj >> /XObject << endobj Determine the suitable material for each of the component. << What is the purpose of the cyclic control stick? << /CS0 [/ICCBased 287 0 R] 16 0 obj /K 54 << /S /Artifact /A 414 0 R /Filter /FlateDecode /Lang (EN-GB) /Pg 35 0 R /Sh4 322 0 R << /Lang (EN-GB) 14 132 0 R 16 133 0 R 18 134 0 R 20] /Count 0 endobj /Fm0 295 0 R Using a 2mm self tap screw, access the rear bracket hole and tap a drill hole for the rear bracket. /A 449 0 R /Pg 42 0 R 46 0 obj By continuing here you are consenting to their use. /ordmasculine 188 /onequarter /onehalf /threequarters 192 /Agrave /Aacute /Acircumflex /Atilde /S /Normal >> /S /Normal /P 433 0 R endobj << /A 596 0 R Modify the DayOfYear class, written in the previous question, to add a constructor that takes two parameters: a string representing a month and an integer in the range 0 through 31 representing the day of the month. << Thin sheets of the material can be stacked in various ways to meet specific strength or . /Contents 366 0 R endobj /Contents 364 0 R >> >> 218 0 obj /Contents 360 0 R /TT4 314 0 R /CropBox [0.0 0.0 595.32 841.92] /Lang (EN-GB) >> >> /Lang (EN-GB) /Type /MCR /MediaBox [0.0 0.0 595.32 841.92] /A 589 0 R 183 0 obj situs link alternatif kamislot helicopter frames consist of the fuselage /P 608 0 R The frame is made from very strong . /K 5 Thankfully, Igor Sikorsky had the idea to install a tail rotor to counter this torque reaction and provide directional control. >> /A 460 0 R /CS1 [/ICCBased 306 0 R] /TT1 289 0 R /Pg 35 0 R /Lang (EN-GB) >> The latter two are still in use. /Sh12 342 0 R CONTROLLED FLAMBING ANTI-CRASH COMPOSITE STRUCTURE FOR AIRCRAFT. 141 0 obj A typical helicopter fuselage structure shown in Fig 1 consists of several key components: (a) Subfloor box, (b) Energy absorbing beam, (c) Box beam frame members, (d) Longitudinal beam, and (e) Outer fuselage skin. /Lang (EN-GB) /Pg 43 0 R /A 409 0 R D:20170502160949 131 0 obj 74 0 R 75 0 R 76 0 R 77 0 R 78 0 R 79 0 R 80 0 R 81 0 R 82 0 R 83 0 R /Pg 35 0 R /MediaBox [0.0 0.0 595.32 841.92] 117 0 obj The semirigid rotor system in Figure 4 makes use of a teetering hinge at the blade attach point. /S /Subscript /Pg 33 0 R >> endobj /Pg 35 0 R << /S /Tabelle_content /P 567 0 R /Sh13 343 0 R /P 497 0 R /ColorSpace << /K 148 >> /S /P /DropCap /Figure endobj /C2_0 365 0 R /K 165 /P 256 0 R /Pg 36 0 R 165 0 obj >> endobj >> /P 17 0 R /TT1 313 0 R /Pg 35 0 R << 126 0 obj /TT1 289 0 R /Subtitle#2CFig /H2 >> /CS1 [/ICCBased 306 0 R] /Contents 361 0 R << /Lang (EN-GB) /P 17 0 R /K [417 0 R 418 0 R 419 0 R 420 0 R 421 0 R 422 0 R 423 0 R 424 0 R 425 0 R 426 0 R /Pg 33 0 R /K 9 There are also accessories and controls that go with these structures. /S /Tabelle_content Definition of a Helicopter. endobj /S /Strong /P 642 0 R /S /formula /Rotate 0 Customer satisfaction 4,2/5. /Pg 35 0 R /S /L /Lang (EN-GB) /P 532 0 R >> /S /Normal /Pg 35 0 R >> << << -Line about which a rotating body turns >> /Lang (EN-GB) << >> >> /Pg 35 0 R >> 74 0 obj /A 656 0 R 204 0 obj endobj /Fm2 297 0 R endobj 168 0 obj endobj endobj /A 627 0 R endobj http://www.zotero.org/styles/harvard1 << >> >> endobj /K 1 /GS0 307 0 R /P 586 0 R All these load cases, and the interaction between cases must be considered to arrive at a final design. For instance, 53 percent of the aircraft consists of carbon-fiber composite parts. /Pg 30 0 R >> >> /S /Tabelle_content -when the angle of attack decreases, center of pressure moves rearward, Direction of airflow opposite the direction of the rotating blades, Angle created between the chord Line of the airfoil and the relative wind /P 648 0 R 266 0 obj Give the reason why the material is selected. Tail drive shaft For design and analysis, engineers group parts which have the same function into systems. endobj /Lang (EN-GB) >> /K 46 166 0 obj >> /Pg 35 0 R >> /XObject << /K 110 endobj /Type /Metadata /Subtype /XML /StructParents 0 /Lang (EN-GB) The fuselage is the name given to the main body of the aircraft and houses the pilots, crew, passengers, and cargo. << /Lang (EN-GB) /Lang (EN-GB) /S /Tabelle_content /K 160 endobj /A 392 0 R /P 601 0 R /TT0 313 0 R /S /Tabelle_content 138 0 obj 145 0 obj 263 0 obj /Fm1 296 0 R The invention relates to a helicopter fuselage of the type including a central structure to which are linked a front structure, a rear structure and a landing gear, and which supports a transmission gearbox, a main rotor and at least one engine (50), and of the type in which the central structure includes a skeleton (16) fitted with covering elements which define the external shape of the . For example, rotorcraft consist of engines, rotors, drive shafts, /S /Tabelle_content /TT0 290 0 R 114 0 obj >> >> >> /Producer (Adobe PDF Library 15.0) /Pg 35 0 R /XObject << These external pressure loads combine with internal pressure loads if the aircraft is pressurized. The semi-monocoque construction, which is virtually standard in all modern aircraft, consists of a stressed skin with added stringers to prevent buckling, attached to hoop-shaped frames. /Lang (EN-GB) /A 384 0 R 154 0 obj /Lang (EN-GB) /Lang (EN-GB) << /TT0 290 0 R /D [41 0 R /XYZ 104 267 0.0] Most have the pilot seated on the right side, although there are some with the pilot seated on the left side or center. /A 393 0 R /K 30 NOTAR is an acronym that stands for no tail rotor. As the speed of the main rotor changes, the speed of the NOTAR fan changes. endobj /Pg 41 0 R /Pg 26 0 R /K 7 Foot pedals A pair of foot pedals controls the tail rotor. /Parent 4 0 R /Lang (EN-GB) 134 0 obj 57 0 obj endobj >> /K 8 /K 17 endobj /A 401 0 R >> >> One of the helicopters came down and major components/assemblies were recovered . endobj >> /Pg 41 0 R /Pg 36 0 R /GS0 307 0 R /XObject << /Shading << /Chart /Figure endobj Aluminum wasn't widely used in aeronautical applications until the early 1920s, but its appearance helped engineers make their helicopters lighter and, as a result, easier to fly. /K 11 >> /A 463 0 R /Rotate 0 << 167 0 obj /Fm3 298 0 R endobj << 220 0 obj endobj endobj /P 17 0 R 87 0 obj >> /P 423 0 R >> endobj /Parent 13 0 R >> /Lang (EN-GB) /K 116 /Rotate 0 /Pg 35 0 R /K 17 0 R Enthusiats at your service : at 1001hobbies, we share your endobj /K 122 <> >> /K 2 /Fm4 299 0 R >> /First 11 0 R << >> /ColorSpace << endobj endobj endobj /K 2 /Type /Page /K 56 >> helicopter frames consist of the fuselage. /K 8 143 0 obj /S /Tabelle_content << endobj >> /Fm0 295 0 R /K 3 /acircumflex /atilde /adieresis /aring /ae /ccedilla /egrave /eacute /ecircumflex /edieresis endobj /Lang (EN-GB) /ExtGState << /A 388 0 R 92 0 obj During the early days of aviation, primitive fuselages were built with wood. 3 0 obj /Lang (EN-GB) endobj /CropBox [0.0 0.0 595.32 841.92] endobj /Lang (EN-GB) /K 15 In many models, a frameless plastic canopy surrounds the pilot and connects in the rear to a flush-riveted aluminum frame. In addition, the purpose of an airplane goes a long way in the manufacturers' decision to use a particular type of metal, especially the metal used in the plane's frame and body. /S /Artifact /Pg 33 0 R /Lang (EN-US) >> /Fm2 297 0 R endobj /P 603 0 R /ColorSpace << 248 0 obj >> /A 520 0 R /A 391 0 R endobj /S /Normal /Pg 26 0 R >> /S /Span /Sh2 350 0 R << /K 141 /Pg 42 0 R /Contents 335 0 R /Fm1 296 0 R endobj >> 2017-05-08T21:10:34+01:00 /TT0 290 0 R <> >> /K 74 /S /Tabelle_content << endstream endobj 53 0 obj <> endobj 54 0 obj <>/Font<>/ProcSet[/PDF/Text]/Properties<>>>/Rotate 0/Type/Page>> endobj 55 0 obj <>stream /GS1 308 0 R >> /Pg 42 0 R << /K 173 /Differences [24 /breve /caron /circumflex /dotaccent /hungarumlaut /ogonek /ring /tilde 39 /Kids [24 0 R 25 0 R 26 0 R 27 0 R] /K 157 37 0 obj /K [0 127 0 R 6 128 0 R 8 129 0 R 10 130 0 R 12 131 0 R /K 41 /S /Normal In twin-rotor helicopters, the torque produced by the rotation of the front rotor is offset by the torque produced by a counter-rotating rear rotor. /Pg 35 0 R The relative windspeed is greater on an advancing blade than it is on a retreating blade. Airframe design encompasses engineering, aerodynamics, materials technology, and manufacturing methods to achieve favorable balances of performance, reliability, and cost. /A 441 0 R 268 0 obj /CS0 [/ICCBased 287 0 R] /Lang (EN-GB) /S /P >> endobj >> /Pg 30 0 R >> /S /P /Lang (EN-GB) /A 477 0 R << /Pg 35 0 R >> /GS0 288 0 R /Type /Outlines 33 0 obj 255 0 obj /ZaDb 10 0 R Provides data that is required by the CIPS unit for blade tracking analysis, Mounted accelerometers on or around the component under test provide to the CIPS the data required to calculate a balance or soothing solution, Helicopter flying handbook, ch 1-3 intro / Ae, Introduction to Chemical Engineering Thermodynamics, Hendrick Van Ness, J.M. /Lang (EN-GB) << /Tabs /S /A 464 0 R /Lang (EN-GB) /K 4 >> /TT2 314 0 R << /K 42 Structural analysis) /K 36 endobj /S /P /P 17 0 R /Lang (EN-GB) >> /P 17 0 R /Pg 33 0 R << >> 169 0 obj /K 146 >> 252 0 obj /Pg 30 0 R /ExtGState << Large frames are required at the wing-fuselage and tail-fuselage interface to transmit the loads generated by these lifting surfaces into the fuselage. /Lang (EN-US) According to Wikipedia, the semi-monocoqne fuselage structure is preferred when constructing an all-aluminum fuselage. endobj /Lang (EN-GB) /Parent 4 0 R 122 0 obj /TT2 311 0 R >> http://www.zotero.org/styles/american-medical-association /A 489 0 R /S /Span << /Lang (EN-GB) >> >> /Pg 33 0 R /Subscript /Span >> << endobj >> 107 0 obj /Resources << /Kids [28 0 R 29 0 R 30 0 R 31 0 R 32 0 R 33 0 R] /ColorSpace << IEEE >> >> 96 0 obj /Subtype /Type1 endobj /Pg 35 0 R Additionally, the remainder of the air from the fan is sent through the tail boom to a vent on the aft left side of the boom where it is expelled.