GATE Aerospace Engineering Detailed Syllabus
GENERAL APITITUDE
VERBAL ABILITY
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English grammar , sentence completion
, Verbal Analogies , Word Groups , Instructions , Critical Reasoning and
Verbal Deductions .
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NUMERICAL ABILITY
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Numerical Computation , Numerical
Estimation , Numerical Reasoning and Data Interpretation .
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AEROSPACE ENGINEERING
SECTION 1 : ENGINEERING
MATHEMATICS
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CORE TOPICS
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LINEAR EQUATIONS
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Vector Algebra , Matrix Algebra ,
System Of Linear Equation , Rank Of Matrix ,
Eigenvalues and
Eigenvectors .
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CALCULUS
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Functions Of Single Variables ,
Limits , Continuity and Differentiability , Mean Value Theorem , Chain Rule ,
Partial Derivatives , Maxima and Minima , Gradient , Divergence
and Curl , Directional Derivatives , Integration , Line , Surface
and Volume Integrals , Theorems Of Stokes , Gauss and Green .
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DIFFERENTIAL EQUATIONS
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First Order Linear and Nonlinear
Differential equation , Higher Order Linear ODEs with Constant Coefficients ,
Partial Differential Equations and Separation Of Variable Methods .
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SPECIAL TOPICS
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Fourier Series , Laplace Transforms ,
Numerical Methods For Linear Equations and Nonlinear Algebraic Equations ,
Numerical Integration and Differentiation .
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SECTION 2: FLIGHT MECHANICS
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CORE TOPICS
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BASICS
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Atmosphere: Properties, standard
atmosphere. Classification of aircraft. Airplane (fixed wing aircraft)
configuration and various parts
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AIRPLANE PERFORMANCE
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Pressure
altitude; equivalent, calibrated, indicated air speeds;
Primary flight instruments: Altimeter,
ASI, VSI, Turn-bank indicator. Drag polar; takeoff and landing; steady climb
& descent, absolute and service ceiling; cruise, cruise climb, endurance
or loiter; load factor, turning flight, V-n diagram Winds: head, tail &
cross winds;
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STATIC STABILITY
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Angle of attack, sideslip; roll,
pitch & yaw controls; longitudinal stick fixed & free stability,
horizontal tail position and size; directional stability, vertical tail
position and size; dihedral stability. Wing dihedral, sweep & position; hinge
moments, stick forces;
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SPECIAL TOPICS
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Dynamic stability: Euler angles;
Equations of motion; aerodynamic forces and moments, stability & control
derivatives; decoupling of longitudinal and lateral-directional dynamics;
longitudinal modes; lateral-directional modes.:
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SECTION 3: SPACE DYNAMICS
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CORE TOPICS
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Central force motion, determination
of trajectory and orbital period in simple cases
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SPECIAL TOPICS
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Orbit transfer, in-plane and
out-of-plane
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SECTION 4: AERODYNAMICS
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CORE TOPICS
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BASIC FLUID MECHANICS
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Conservation laws: Mass,
momentum (Integral and differential form);
Potential flow theory: sources, sinks, doublets, line vortex and
their superposition; Viscosity, Reynolds number.
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AIRFOILS AND WINGS
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Airfoil nomenclature;
Aerodynamic coefficients: lift, drag and moment; Kutta-Joukoswki theorem;
Thin airfoil theory, Kutta condition, starting vortex; Finite
wing theory: Induced drag, Prandtl lifting line theory; Critical and drag
divergence Mach number.
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COMPRESSIBLE FLOWS
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Basic concepts of compressibility,
Conservation equations; One dimensional compressible flows, Fanno flow,
Rayleigh flow; Isentropic flows, normal and oblique shocks, Prandtl-Meyer
flow; Flow through nozzles and diffusers.
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SPECIAL TOPICS
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Elementary ideas of viscous flows
including boundary layers; Wind Tunnel Testing: Measurement and
visualization techniques.
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SECTION 5: STRUCTURES
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CORE TOPICS
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STRENGTH OF MATERIALS
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States of stress and strain. Stress
and strain transformation. Mohr's Circle. Principal stresses.
Three-dimensional Hooke's law. Plane stress and strain; Failure theories:
Maximum stress, Tresca and von Mises; Strain energy. Castigliano's
principles. Analysis of statically determinate and indeterminate trusses and
beams. Elastic flexural buckling of columns.
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FLIGHT VEHICLE STRUCTURES
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Characteristics of aircraft
structures and materials. Torsion, bending and flexural shear of thin-walled
sections. Loads on aircraft.
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STRUCTURAL DYNAMICS
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Free and forced vibrations of
undamped and damped SDOF systems. Free vibrations of undamped 2-DOF systems.
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SPECIAL TOPICS
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Vibration of beams.
Theory of elasticity: Equilibrium and
compatibility equations, Airy’s stress function
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Also Download Previous Year Question Paper of Click The Link Below
GATE Aerospace Engineering 2017 Question Paper
SECTION 6: PROPULSION
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CORE TOPICS
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BASICS
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Thermodynamics, boundary layers and
heat transfer and combustion thermo chemistry.
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THERMODYNAMICS OF AIRCRAFT ENGINES
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Thrust, efficiency and engine
performance of turbojet, turboprop, turbo shaft, turbofan and ramjet engines,
thrust augmentation of turbojets and turbofan engines. Aerothermodynamics of
non-rotating propulsion components such as intakes, combustor and nozzle.
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AXIAL COMPRESSORS
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Angular momentum, work and
compression, characteristic performance of a single axial compressor stage,
efficiency of the compressor and degree of reaction.
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AXIAL TURBINES
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Axial turbine stage efficiency
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CENTRIFUGAL COMPRESSOR
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Centrifugal compressor stage
dynamics, inducer, impeller and diffuser.
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ROCKET PROPULSION
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Thrust
equation and specific impulse, vehicle acceleration, drag, gravity losses,
multi-staging of rockets. Classification of chemical rockets, performance of
solid and liquid propellant rockets.
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