3rd International Conference on Trends in Mechanical and Industrial Engineering (ICTMIE ’2013) January 8-9‚ 2013 Kuala Lumpur (Malaysia) Conceptual Design of Short Takeoff Supersonic Aircraft with Cold Flow Nozzles Vignesh. M 1‚ Sathish. K1‚ Adrin Issai Arasu. L1‚ Dharun Lingam. K1‚ and Sanal Kumar. V.R 2 consumption and poor range) in turn making it unprofitable for manufacturers to produce these kinds of aircraft. It can cover a distance from India to USA in 2 ½ hours. Propulsion systems that
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Module of product design and total quality management for aviation industry‚ aviation maintenance industry‚ pilots and students of aviation management Superior University Product Design and Development / TQM Module Handbook Contents 1. Staff and Course Delivery Arrangements 03 2. Course Introduction 03 3. Course Objective 04 4. Course Coverage 04 5. Student Gains 06 6. Teaching
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INTRODUCTION Traffic jams are the bane of any commuter. Many of us spend an hour or so stuck in traffic every week. The growing population is partly to blame for our congested roads‚ but the main problem is that we are not expanding our transportation systems fast enough to meet ever increasing demands. One solution is to create a new type of transportation that doesn’t rely on roads‚ which could one day make traffic jams a 20th century relic. To do this‚ we must look to the sky and water. WHY
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speeds. Wing taper reduces the effectiveness of winglets because of the lower outboard wing loading with taper. Wing taper may also affect the optimum angle of attack for lift to drag improvements. For optimum winglet effectiveness‚ an untampered airfoil must be used. At low speeds‚ a symmetric winglet is at least as effective as a supercritical section winglet. So‚ there is no reason to use the more difficult to construct supercritical shaped winglet. It is found that there is no need to sweep the
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BRUNEL UNIVERSITY SCHOOL OF ENGINEERING AND DESIGN INCREASING THE SKYRANGER’S AERODYNAMIC PERFORMANCE THROUGH SHAPE OPTIMISATION OF THE WING KENNEDY KAIRU MBUGUA 0803460 SUPERVISOR: RAY KIRBY ME3309 Overview of the Project The Skyranger along with other ultra-light home build plane are designed and constructed to be extremely cost effective due to the low price at which they are marketed. In this report the aerodynamic performance of the Skyranger’s wing is analysed and particular
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www.jntuworld.com R07 Code No: 07A82104 Set No. 2 IV B.Tech II Semester Examinations‚AUGUST 2011 HELICOPTER ENGINEERING Aeronautical Engineering Time: 3 hours Max Marks: 80 Answer any FIVE Questions All Questions carry equal marks 1. (a) Describe with sketches and plots the difference between a conventional airplane and Helicopter. Emphasize on the generation of lift in both cases. (b) Explain with sketches and plots the requirement of tail rotor in a conventional single rotor
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upper and lower surfaces of the airfoil‚ lift and drag per span. (Hint: 2 2∞ ∞ ∞ q = p M γ ‚ γ=1.4) 2 Q3. a- A thin symmetrical supersonic airfoil has parabolic upper and lower surfaces with a maximum thickness occurring at midchord. Using linearized theory‚ compute the lift to drag ratio when it is set at an angle of attack of 5º. Figure 5 [Hint: y = A+ B (αx) + C (αx)2‚ and dx ε = dy ] Q4. Estimate the critical Mach number for NACA 0012 airfoil at 10º angle of attack. The pressure
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The Saab 340A is a Swedish twin turboprop passenger plane which was first produced in 1983. Although they are no longer in production‚ they are still actively used. It was designed in a partnership between Saab and Fairchild with each company being responsible for certain aspects. Fairchild’s portin included the wings‚ engine housing‚ and empennage‚ while Saab handles the fin‚ fuselage‚ and final assembly. They agreed upon a General Electric CT7-5A2 engine and a Dowty Rotol 4 Bladed Composite propeller
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An airplane or aeroplane (informally plane) is a powered fixed-wing aircraft that is propelled forward by thrust from a jet engine or propeller. Airplanes come in a variety of sizes‚ shapes‚ and wing configurations. The broad spectrum of uses for airplanes includes recreation‚ transportation of goods and people‚ military‚ and research. Most airplanes are flown by a pilot on board the aircraft‚ but some are designed to be remotely or computer-controlled. Etymology and usage First attested in
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measurement of a VAWT in skew. AIAA/ASME Wind Energy Symposium (2006). 55. Sørensen JN‚ Shen WZ and Mikkelsen R. Wall correction model for wind tunnels with open test section‚ AIAA Journal 2006; 44‚ n.8. 56. Claessens MC. The design and testing of airfoils for application in small vertical axis wind turbines. MSc Thesis dissertation 2006. Delft University of Technology‚ The Netherlands. 57. Sant T. Improving BEM based aerodynamic models in wind turbine design codes. PhD Thesis dissertation 2007‚ Delft
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