[PDF] Top 20 J. Aerosp. Technol. Manag. vol.4 número4
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J. Aerosp. Technol. Manag. vol.4 número4
... At the end of the 1970s, the Complete Brazilian Space Mission – MECB established the goal to develop a national satellite to be launched, by a launch vehicle designed and manufactured [r] ... See full document
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J. Aerosp. Technol. Manag. vol.4 número4
... Turbulence measurements were performed for the free- stream velocity of, approximately, 40m/s. Mean velocity SUR¿OHVDQGWXUEXOHQFHLQWHQVLW\OHYHOVZHUHREWDLQHGXVLQJ a constant temperature hot-wire anemometer, from ... See full document
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J. Aerosp. Technol. Manag. vol.4 número4
... The method for preparing a hypergolic composition for rocket propellant comprises adding a gelling agent to the liquid fuel and suspending a particulate ignition agent i[r] ... See full document
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J. Aerosp. Technol. Manag. vol.4 número4
... The control logic takes into consideration that the reading operation executed by the RMAP block is performed in bursts (of con¿ gurable size), raising the ef¿ - cie[r] ... See full document
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J. Aerosp. Technol. Manag. vol.4 número4
... YROWDJHDSSOLHGWRWKHÀRZYHORFLW\LQGXFHGE\WKHDFWXDWRU 7KH\REVHUYHGWKDWWKHFKRLFHRIGLHOHFWULFPDWHULDODIIHFWV WKH SODVPD YROXPH WKH GLVWULEXWLRQ RI HOHFWULF ¿HOG OLQHV JRYHUQHGE\WKHGLHOHFWULFF[r] ... See full document
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J. Aerosp. Technol. Manag. vol.4 número4
... WRPLOOLRQ,WFDQEHLQIHUUHGWKDWWKHYHORFLW\YDULDWLRQ by itself is small enough to introduce any effect of Reynolds number on lift curve slope and stall angle of the aircraft. ... See full document
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J. Aerosp. Technol. Manag. vol.4 número4
... Abstract: Deployable structure technology has been used in aerospace and civil engineering structures very popularly. This paper reported on a recent development of numerical approaches [r] ... See full document
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J. Aerosp. Technol. Manag. vol.4 número4
... Analyser 47$,QVWUXPHQWV86$7KHGLIIHUHQWH[SHULPHQWVZHUH performed on dual cantilever clamp varying the frequency, temperature, stress, and strain ... See full document
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J. Aerosp. Technol. Manag. vol.4 número4
... dispersion factors to be considered. Studies that evaluate the accuracy of the missile datcom compared to experimental wind tunnel data shows that the results for aerodynamic drag are predicted by missile datcom with an ... See full document
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J. Aerosp. Technol. Manag. vol.4 número4
... conditions to the experimental setup. One-side welding temperature and mechanical response were simulated with power of 1,400 W and a speed of 3 m/min. For the simulation of two-side weld, the chosen parameters were ... See full document
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J. Aerosp. Technol. Manag. vol.4 número4
... WKH PHDVXUHG VSHFWUXP ZLWK D VLPSOL¿HG V\QWKHWLF RQH considering only the sample constituent element. The synthetic spectrum was built by adding lorentzian curves with peak values given by the Einstein ... See full document
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J. Aerosp. Technol. Manag. vol.4 número2
... is a subset of the GBAS signal-in-space integrity risk, where the protection level integrity risk (3.6.7.1.2.2.1) has been excluded and the effects of all other GBAS, SBAS and core satel[r] ... See full document
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J. Aerosp. Technol. Manag. vol.4 número2
... IRXU J\URV LQ D WHWUDG FRQ¿JXUDWLRQ 7KH SURFHGXUH KDV WDNHQ into account a technique based on least-square methods and wavelet denoising to perform the best estimate RI WKH VHQVRU D[LV ... See full document
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J. Aerosp. Technol. Manag. vol.4 número2
... However, since in the case of aircraft f light dynamics this differential f latness property is implicit, a neural network is introduced to deal with its numerica[r] ... See full document
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J. Aerosp. Technol. Manag. vol.4 número2
... The loss model is established by means of applying boundary layer theories, basic thermodynamic equations, and VLPSOL¿HGHTXDWLRQRIFRQVHUYDWLRQRIPDVVPRPHQWXPDQG ... See full document
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J. Aerosp. Technol. Manag. vol.4 número2
... Since trajectory design of a launch vehicle requires prior knowledge of the masses and propulsion performance parameters of the Micro Air Launch Vehicle, whereas the vehicle design requ[r] ... See full document
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J. Aerosp. Technol. Manag. vol.4 número2
... $ FRPSXWDWLRQDO VRIWZDUH FDOOHG 0$7/$% KDV EHHQ used to carry out numerical simulations of differential and DOJHEUDLF(TVWRJRYHUQLQJWKHSURSHOODQWÀRZGXULQJ YDFXXP FDVWLQJ 0DWKHZV DQG )LQN ... See full document
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J. Aerosp. Technol. Manag. vol.4 número1
... ,QWKLVVHFRQGWHVWFDVHWKHVDWHOOLWHLVFRPPDQGHGWRFKDQJH LWVDWWLWXGHLQLWLDOO\ZLWKWKUHHDQJOHVUROOSLWFKDQG\DZDW WKHVDPHYDOXHRIIRUDQHZDWWLWXGHGH¿QHGE\WKHYDOXHV ... See full document
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J. Aerosp. Technol. Manag. vol.4 número2
... The International Commission on Radiological Protection (ICRP) recognizes the need to control the exposure of the SHUVRQUHSUHVHQWLQJWKHÀLJKWSURIHVVLRQDOJURXSOLNHSLORWV and cre[r] ... See full document
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J. Aerosp. Technol. Manag. vol.4 número2
... States of America (Whiteman et al7KHH[DPLQD- tion of radiosonde data in cases with and without jet has a GLIIHUHQWVSHFL¿FKXPLGLW\DYHUDJHRIDERXWJNJ7KH transport performed of the LLJ ... See full document
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