Journal of Aerospace Engineering & Technology
Volume 10, Issue 2 (2020)
Published
Table of contents
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Hydrodynamic Stability of Parallel Flow and Rotating Flow of Inviscid Fluid Dynamics
Abstract: AbstractStream unsteadiness and fierce change can be all around clarified utilizing another proposedhypothesis - Energy slope hypothesis (Dou, 2005). In this hypothesis, the strength of a streamrelies upon the general size of vitality slope in streamwise heading and that transverse way, ifthere is no work input. In this note, it is indicated dependent on the vitality slope hypothesisthat inviscid non-uniform stream is flimsy if the vitality transverse way isn't consistent. …
Published in Journal of Aerospace Engineering & Technology · Vol. 10, Issue 2, 2020 · pp. 1–14 Read article
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Precise Numerical Calculation of the Bond Number of a Fluid Drop and of the Surface Tension Coefficient at the Fluid-Gas Interface
Abstract: Precise calculation of the Bond number of a fluid drop and the surface tension coefficient at the fluid-gas interface plays an important role in modeling of the behavior of fluids in aircraft fuel tanks during overloads resulting from flight and the behavior of fluids in power supply and life support systems of spacecraft and space stations. The existing methods of calculation of the Bond number of a fluid drop and …
Published in Journal of Aerospace Engineering & Technology · Vol. 10, Issue 2, 2020 · pp. 15–22 Read article
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Advancements in De-icing and Anti-icing Technologies used in Aircraft
Abstract: In today’s fast progressing world, there is an advent of technology in all spheres of life. One such area that has grown by leaps and bounds is that of aircraft technology and the systems involved in it. This paper focuses mainly on the technologies/systems used for De-icing and Anti-icing applications in aircrafts (specifically those with fixed wings), be it manned or unmanned (UAVs). Icing and frosting of wings are a …
Published in Journal of Aerospace Engineering & Technology · Vol. 10, Issue 2, 2020 · pp. 23–32 Read article
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Projections of Natural Absorption in Three-Dimensional Behind Phase into Turboprop Circulation
Abstract: Designed to enhance fuel-air mixing at supersonic speeds is one of the most difficult issues in the design of scramjet engine combustors. Various experiments and investigations were considered to boost fuel-air mixture in supersonic air streams. In this analysis, phase effects on transverse gaseous hydrogen injection into supersonic crossflow are examined numerically. Three-dimensional Reynolds Combined Navier-Stokes equations and k- sst turbulence model and perfect gas equation were numerically solved. Current …
Published in Journal of Aerospace Engineering & Technology · Vol. 10, Issue 2, 2020 · pp. 33–40 Read article
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Introduction of JET ENGINE and type of jet engine.
Abstract: The conventional jet engine is optimized to produce high thrust and low specific fuelconsumption. The changes are made in compressor which is responsible for the pressure raise in the total process. The compressor section is replaced with two smaller compressors which are parallel to each other with separate individual inlets. It is designed that the two compressors do compression separately and produce high pressure raise. This pressure raise will reduce …
Published in Journal of Aerospace Engineering & Technology · Vol. 10, Issue 2, 2020 · pp. 41–46 Read article