Thermal engineering can be defined as controlling the heating or cooling processes in an environment involving various techniques. Thermal engineering has engulfed our lives from a very primitive stage without our knowledge. It has been a part of human development since the 1600s, but came into existence when James Watt patented steam engine in 1781. Though we have gladly accepted this invention and moved away from this towards economic development in the form of the industrial revolution, advanced transportation modes, protracted growth and greater connectivity, thus shifting mankind from one revolution after another. Amidst all the inventions and discoveries we failed to acknowledge this field of science in our daily lives; however, its herculean significance comes without any doubt. Hence, there is a growing enthusiasm to pursue this field of engineering among students across the globe.
Thermal engineering is encompassed with subjects like; mass transfer, heat transfer, fluid mechanics, turbo dynamics, thermodynamics, cryogenic engineering, instrumentation in thermal systems, renewable energy systems, energy system modelling and analysis, turbo compressors, steam and gas turbines, heat exchange, fire dynamics and engineering. With so many subjects to study, it becomes difficult for the students to write the assignments. Therefore, we provide thermal engineering assignment help at a very nominal price.
The scope of thermal engineering as in the previous days is not only confined with engines, but has grown by leaps and bounds. Thermal engineering applicability has increased and so has the subject’s scope. Its wide areas of applications include;
Apart from the above mentioned usages thermal engineering is also used for generating renewable energy in various countries. In our thermal engineering assignment help service, our adept writers provide the best solutions to all your assignment problems with proper referencing.
There are numerous questions answered by our thermal engineering experts on a regular basis. Some common questions serviced time and again are; elaborate in detail about parallel flow heat exchanger, what is monochromatic emission power? Explain reflectivity, Newton’s law of convection, etc. Our writers provide solutions to all theoretical and problematic questions – no matter the level of difficulty. They provide the proper referencing as required by your university.
To solve a thermal engineering problem, the use of few subjects is pivotal. They are used separately or in combination to draw the desired outcome. The major topics in thermal engineering are;
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For small flow rates, the volume flow rate Q through a small triangular-section tube of side W and length L is a function of dynamic viscosity , pressure drop per unit length p/L and W. Using Buckingham pi theorem, express the relation between variables in a non-dimensional form .
The first part should be solved manually, and the second part should be done by using abaqus software. Consider a first-order triangular element, if we know the coordinates (x,y) and the displacements (u,v) at the nodes as follows: Node 1: (x1, y1) = (3.0,3.0), (u1, v1) = (0.012,0.006) m Node 2: (x2, y2) = (2.0,4.0), (u2, v2) = (0.015,0.005) m Node 3: (x3, y3) = (1.0,1.0), (u3, v3) = (0.010,0.008) m a) Find the interpolation functions for this element. b) Calculate the displacements (u, v) at the points (4, 3) and (3, 2).
Design an efficient retaining wall to be used along the rear of excavated area of the tank. Depending on depth of cut and height of soil to retain,dimensions for both stocky and slender retaining wall will be designed. Retaining walls will be designed to resist against three major failure modes including overturning, sliding and bearing. Based on the design of retaining walls to resist mentioned failure modes, optimal dimensions for the most economical shape of retaining wall will be proposed.
Determine the deflections and stresses in a loaded Pilatus PC/9 wing using finite element computational modelling. The aircraft wing can be simplified using appropriate beam-plate representations. You must decide how to represent the wing to provide meaningful results. This is a major focus of the assignment and much detail and explanation is expected for all choices in your numerical calculations.
The aerodynamic lift of the wing is described by the distributed load of 2w x 300 1 0.04 N/m. The mass of the wing is 27 Kg, and its center of mass is located 2 m from the wing root R. (a) Determine the magnitude of the force and the moment about R exerted by the lift of the wing. (b) Determine the reactions on the wing at R.
Few tasks related to different cipher processes, from ancient Caesar cipher to digital signature of files. This is a great way to practice and fully comprehend concepts of hash, public key, private key and cracking and encryption. In this case we based some of the task on Linux commands and the rest required only simple math calculations
Explain in your own words the purpose of the command in the context of the assignment question. Also, you need to explain in your own words all terminology used—as if you were explaining to an average user. Show that the command worked—either from its output or the output from another command. To capture text output from programs you will have to redirect the output to a file or use the command script.
Design and implement a secured network infrastructure that ensures high availability, reliability, scalability, performance and security to support GB services. This requires 1) the design of the network; 2) the delivery of a comprehensive network security plan; and 3) Security technology implementation - proof of concept.
You are required to design a simple CMOS circuit consisting of a two-input NOR gate. You are required to show the layout (plan view) of the circuit, after calculating the aspect ratio (W?L) of the transistors. The Layout of the circuit includes the VDD and ground lines.