{"id":1861,"date":"2016-12-02T07:06:29","date_gmt":"2016-12-02T07:06:29","guid":{"rendered":"http:\/\/www.inspirenignite.com\/anna-university\/?p=1861"},"modified":"2019-07-18T06:25:35","modified_gmt":"2019-07-18T06:25:35","slug":"anna-university-b-tech-ae-r13-5th-flight-dynamics-detailed-syllabus","status":"publish","type":"post","link":"https:\/\/www.inspirenignite.com\/anna-university\/anna-university-b-tech-ae-r13-5th-flight-dynamics-detailed-syllabus\/","title":{"rendered":"Anna University B.Tech AE (R13) 5th Flight Dynamics Detailed Syllabus"},"content":{"rendered":"

Flight Dynamics Syllabus for B.Tech 5th sem is covered here. This gives the details about credits, number of hours and other details along with reference books for the course.<\/p>\n

The detailed syllabus for Flight Dynamics B.Tech (R13) fifthsem is as follows<\/p>\n

OBJECTIVES<\/strong><\/p>\n

To study the performance of airplanes under various operating conditions and the static and\u00a0dynamic response of aircraft for both voluntary and involuntary changes in flight conditions<\/p>\n

UNIT I : CRUISING FLIGHT PERFORMANCE \u00a0 \u00a0<\/strong> \u00a0 \u00a0 \u00a0 \u00a0 [9 hours]
\nForces and moments acting on a flight vehicle – Equation of motion of a rigid flight vehicle – Different\u00a0types of drag \u2013estimation of parasite drag co-efficient by proper area method- Drag polar of vehicles\u00a0from low speed to high speeds – Variation of thrust, power with velocity and altitudes for air breathing\u00a0engines . Performance of airplane in level flight – Power available and power required curves.\u00a0Maximum speed in level flight – Conditions for minimum drag and power required<\/p>\n

UNIT II : MANOEUVERING FLIGHT PERFORMANCE<\/strong> \u00a0 \u00a0\u00a0[10 hours]
\nRange and endurance – Climbing and gliding flight (Maximum rate of climb and steepest angle of\u00a0climb, minimum rate of sink and shallowest angle of glide) -Turning performance (Turning rate turn\u00a0radius). Bank angle and load factor \u2013 limitations on turn – V-n diagram and load factor.<\/p>\n

UNIT III : STATIC LONGITUDINAL STABILITY<\/strong> \u00a0 \u00a0\u00a0[10 hours]
\nDegree of freedom of rigid bodies in space – Static and dynamic stability – Purpose of controls in\u00a0airplanes -Inherently stable and marginal stable airplanes \u2013 Static, Longitudinal stability – Stick fixed\u00a0stability – Basic equilibrium equation – Stability criterion – Effects of fuselage and nacelle – Influence of\u00a0CG location Power effects – Stick fixed neutral point – Stick free stability-Hinge moment coefficient – Stick free neutral points-Symmetric maneuvers – Stick force gradients – Stick _ force per ‘g’ – Aerodynamic balancing.<\/p>\n

Download iStudy\u00a0Android\u00a0App for complete Anna University syllabus, results, timetables and all other updates. There are no ads and no pdfs and will make your life way easier.<\/strong><\/a><\/p>\n

[TOTAL (L:45+T:15): 60 PERIODS]<\/strong><\/p>\n

OUTCOMES<\/strong><\/p>\n