Issue 15

I. S 38 me we B U pro loa mo bou sol unt are ass tha res sub Th An A . Raju et alii, Fr chanics analy re performed ILDING -B L buildin progres overall blem, object ds, materials dels such as ndary condi ved and veri il the results assembled, i embled mod t is repeated ults are prese jected to rigo is building-bl alysis assum attura ed Integri ses for thes in support o Figure 3 : T OCK A PPRO g-block anal sive manne r response de ives, produc , boundary/in finite-eleme tions, and o fied for accu can be verifie ncorporating els are solved until confide nted to exte rous peer re ock analysis ptions can b tà Strutturale, 1 e two bound f the root-ca (b) RCC WLE ypical peak en ACH AND A ysis approac [2]. Such an termined. T ts, resources terface cond nt models o ther approxim racy. The p d by compar component , and the re nce in the re rnal reviewer view. If nece approach pr e challenged 5 (2011) 35-49 ing thermal use investigat (a) D slip-side inbo try temperatur NALYSIS M h begins wi approach pe he hierarchy , schedule, an itions, and t f the individ ations are a rocess at the ison to refer interface con sults are asse sults can be d s and the st ssary, the pr ovides differ and revised ; DOI: 10.3221/I loading cond ion are prese efinition of z ard joggle non e distribution ODELS th basic elem rmits each st of the build d stakehold ools to be u ual compon ssigned to t individual c ence solution ditions, diffe ssed. The p emonstrated akeholders, e ocess may be ent entry po , analysis fi GF-ESIS.15.05 itions (i.e., o nted. ones. -catalytic peak for the Space ents and b ep in the pro ing-block ap ers are defin sed to solve ents are cre he individual omponent le s or test data rent design c rocess at the and advoca ngineering re repeated fro ints for anal ndings can b n-orbit cold temperatures Shuttle wing-le uilds in com cess to be ve proach is pr ed. Second, to problem ated. The m component vel is an iter . Then, the onfigurations assembly lev ted by the an ports are wr m any of the ysts, stakeho e compared and entry pe . ading edge. plexity in a rified and its esented in F the structur are identified aterial mod models, and ative process individual co , and various el is also an alysis team it itten, and th building-blo lders, and ex to observe ak heating) systematic influence on ig. 4. First, al configurat . Next, ana eling proced the models that is repe mponent mo load cases. iterative pro self. Finally, e entire effo ck steps. ternal review d behavior, that and the the ion, lysis ure, are ated dels The cess the rt is ers. and