3.The performance of a MHD-Arc-Scramjet combined cycle engine is analyzed by investigating the effect of energy-bypass system on the engine specific thrust and presenting the difference of the specific thrust between the MHD-Arc-Scramjet combined cycle engine and a conventionalscramjet.以MHD-Arc-Sc...
B. Petit Ramjets and scramjets Encycl. Phys. Sci. Technol., Elsevier (2003), pp. 867-884, 10.1016/B0-12-227410-5/00909-1 View PDFView articleGoogle Scholar [14] A. Gany, Y.M. Timnat Advantages and drawbacks of boron-fueled propulsion Acta Astronaut, 29 (1993), pp. 181-187, 10.1...
Therefore, it is likely that the actual ignition delay difference between the comparison literature is not that large. In conclusion, the chemical reaction mechanism can be used for the numerical simulation of DCR and scramjet. Table 2. Boundary conditions of DCRs and scramjets. 2.2. Physical ...
The performance of a MHD-Arc-Scramjet combined cycle engine is analyzed by investigating the effect of energy-bypass system on the engine specific thrust and presenting the difference of the specific thrust between the MHD-Arc-Scramjet combined cycle engine and a conventionalscramjet. ...
The performance of a MHD-Arc-Scramjet combined cycle engine is analyzed by investigating the effect of energy-bypass system on the engine specific thrust and presenting the difference of the specific thrust between the MHD-Arc-Scramjet combined cycle engine and a conventionalscramjet. ...
In order to remain self-sustained, the profile is attained by the combined operation of a turbojet, ramjet, and scramjet propulsion system. Table 1. Concept aircraft target flight profile. A feasible combination of a dual-mode ramjet-scramjet is given by Figure 2, such that during high-...