1992
DOI: 10.2514/3.46173
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Thermal management for a Mach 5 cruise aircraft using endothermic fuel

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Cited by 42 publications
(10 citation statements)
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“…The V m E values versus the mole fraction of compound content i in the mixture are shown in Figure 1. The values of V m E are negative for the two binary systems of exotetrahydrodicyclopentadiene (1) + n-decane (2) and 1,2,3,4tetrahydronaphthalene (1) + n-decane (2). The minimum values of excess molar volumes are around x 1 = 0.5.…”
Section: ■ Results and Discussionmentioning
confidence: 95%
See 1 more Smart Citation
“…The V m E values versus the mole fraction of compound content i in the mixture are shown in Figure 1. The values of V m E are negative for the two binary systems of exotetrahydrodicyclopentadiene (1) + n-decane (2) and 1,2,3,4tetrahydronaphthalene (1) + n-decane (2). The minimum values of excess molar volumes are around x 1 = 0.5.…”
Section: ■ Results and Discussionmentioning
confidence: 95%
“…As for the binary system of exo-tetrahydrodicyclopentadiene (1) + 1,2,3,4-tetrahydronaphthalene (2), the values of V m E are positive. Since both exo-tetrahydrodicyclopentadiene and 1,2,3,4-tetrahydronaphthalene have ring-like structures, when the two substances are mixed, gaps may appear at the stack site, resulting in a positive excess volume.…”
Section: ■ Results and Discussionmentioning
confidence: 96%
“…On the other hand, the cooling capacity of the total fuel mass in tank can be estimated by the difference between fuel's temperature and threshold temperature, as well as its remaining weight, shown by Equation (9). The cooling capacity of fuel will decrease with the reduced mass and the rising temperature:…”
Section: Residual Cooling Capacity Of Fuelmentioning
confidence: 99%
“…Firstly, it is reported that the overall avionics heat load of the fourth generation aircraft such as the Lockheed Martin F22 reaches over 100 kW [7,8]. Secondly, the aerodynamic heating of a hypersonic vehicle, as mentioned above, will heat the fuselage structure to an extreme temperature, for example, it can exceed 2200 • C on the surface at 5 Ma [9,10], further intensifying the overall heat load. Thirdly, advanced on-board electronic and electrical devices such as the large phased array radar [11] and laser weapons [12,13] are highly integrated and micro-miniaturized [14], where the instantaneous heat load can be up to MW level [15].…”
Section: Introductionmentioning
confidence: 99%
“…With low thermal conductivity, high stiffness to weight ratio, high strength to weight ratio and high temperature mechanical properties, Ti-6Al-4V honeycomb sandwich structures can be 2 of 15 used in aerospace application, such as the thermal protection systems (TPS) components [10]. It can be operated at high temperature up to~440 • C, compared to traditional Aluminum alloys (~300 • C) [11,12]. Hence, the investigation on the mechanical properties of the Ti-6Al-4V honeycomb sandwich structures has drawn much attention in recent decades.…”
Section: Introductionmentioning
confidence: 99%