Aircraft Design detailed Syllabus for Aeronautical Engineering (AERO), R18 regulation has been taken from the JNTUH official website and presented for the students affiliated to JNTUH course structure. For Course Code, Subject Names, Theory Lectures, Tutorial, Practical/Drawing, Credits, and other information do visit full semester subjects post given below. The Syllabus PDF files can also be downloaded from the universities official website.
For all other AERO 3rd Year 2nd Sem Syllabus for B.Tech R18 Regulation JNTUH, do visit AERO 3rd Year 2nd Sem Syllabus for B.Tech R18 Regulation JNTUH Subjects. The detailed Syllabus for aircraft design is as follows.
Pre-requisite:
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Course Objectives:
- Understand the basic skills involved in weight estimation for aircraft conceptual design process.
- Illustrate relevant theoretical knowledge, applicable for initial sizing and configuration layout of aircraft.
- Evaluate basic techniques in literature retrieval and query, also creative and have systematic scientific research methods and working abilities
Course Outcomes:
- Design of aircraft for various application, Effort estimation, Development life cycle
Unit I
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Unit II
Initial Sizing and Configuration Layout: Sizing with fixed engine and with rubber engine. geometry sizing of fuselage, wing, tail, control surfaces, development of configuration lay out from conceptual sketch. the inboard profile drawing, lofting- definition, significance and methods, flat wrap lofting, special consideration in configuration lay out, Isobar tailoring, Sears-Haack volume distribution, structural load paths, radar, IR, visual detectability, aural signature, considerations of vulnerability, crashworthiness, producibility, maintainability, fuselage design, crew station, passengers and payload
Unit III
Propulsion, Fuel System Integration, Landing Gear and Baseline Design Analysis – I: Propulsion selection, jet engine integration, propeller engine integration, engine design considerations, engine size estimation, fuel system design and integration, landing gear and sub systems arrangements, guidelines and significance of design layout, report of initial specifications. Estimation of lift curve slope, maximum lift coefficient, complete drag build up, installed performance of an engine, installed thrust methodology, net propulsive force, part power operation, aircraft structures and loads categories, air load distribution on lifting surfaces, review of methods of structural analysis, material selection, weights and moments statistical group estimation method, centre of gravity excursion control.
Unit IV
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Unit V
Cost Estimation, Parametric Analysis, Optimisation, Refined Sizing and Trade Studies: Elements of life cycle cost, cost estimating method, RDTandE and production costs, operation and maintenance costs, cost measures of merit, aircraft and airline economics, DOC and IOC, airline revenue, breakeven analysis, investment cost analysis, parametric analysis and optimization, improved conceptual sizing methods, sizing matrix plot and carpet plot, trade studies, design trades, requirement trades, growth sensitivities, multivariable design optimization methods, measures of merit, determination of final baseline design configuration, preparation of type specification report. case studies on design of DC-3 and Boeing B-707and747; General dynamics F-16, SR-71 Blackbird, Northrop-Grumman B-2 Stealth Bomber
Text Books:
- Daniel P. Raymer, Aircraft Design: A Conceptual Approachll, AIAA Educational Series, USA, 4th edition, 2006.
- J. F. Marchman, L. R. Jenkinson, Aircraft Design Projects for Engineering students!, AIAA Publishers, USA, 2003.
- Ajoy Kumar Kunda, Aircraft Design!, Cambridge University Press, UK, 2010.
Reference Book:
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For detail Syllabus of all other subjects of B.Tech 3rd Year Aeronautical Engineering, visit AERO 3rd Year Syllabus Subjects.
For all B.Tech results, visit JNTUH B.Tech all years, and semester results from direct links.