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ARO 301: Fluid Dynamics
4.00 Credits
California State Polytechnic University-Pomona
Pressure distribution in a fluid. Control volume and differential approaches to fluid flow analysis. Development and application of NavierStokes equations. Potential flow theory. Dimension analysis and similarity. Viscous flow in ducts. Working knowledge of a highlevel computer language is required. 4 lectures/problemsolving. Prerequisites: ENG 104 or IGE 120 or IGE 121 or IGE 122, C or better in MAT 216. Corequisites: MAT 318, CHE 302, and ME 215.
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ARO 305: LowSpeed Aerodynamics and Performance
4.00 Credits
California State Polytechnic University-Pomona
BoundaryLayer theory. BiotSavart law. Panel methods. Thin airfoil theory. Liftingline theory. Numerical aerodynamics of airfoils and wings. Skin friction drag. Induced drag. Propeller theories. Airplane performance. 4 lectures/ problemsolving. Prerequisite: C or better in ARO 301.
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ARO 305 - LowSpeed Aerodynamics and Performance
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ARO 309: Astronautics and Spacecraft Design
3.00 Credits
California State Polytechnic University-Pomona
Space Environment. Mission design. Lagrange's equation. Kepler's laws, orbits, escape trajectories, interplanetary transfers, gravity assists. Spacecraft propulsion. 3 lectures/problemsolving. Prerequisites: ENG 104 or IGE 120 or IGE 121 or IGE 122, C or better in ME 215.
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ARO 309 - Astronautics and Spacecraft Design
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ARO 311: Gas Dynamics
3.00 Credits
California State Polytechnic University-Pomona
Governing equations of fluid dynamics for compressible flow. Normal shock waves. Oblique shock waves. Expansion waves. Quasionedimensional flow. Fanno flow. Rayleigh flow. Unsteady wave motion. Hightemperature gases and flows. Applications. 3 lectures/problemsolving. Prerequisite: C or better in ARO 301. Corequisite: CHE 302 or ME 301.
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ARO 311 - Gas Dynamics
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ARO 312: Aircraft Jet Propulsion
4.00 Credits
California State Polytechnic University-Pomona
Ideal cycle analysis of ramjet, turbojet, turbofan and turboprop. After burning. Cycle analysis with losses. Nonrotating components: diffusers, nozzles and combustors. Compressor, fans and turbines. Component matching and engine performance. Aircraft engine noise. Hypersonic engines. 4 lectures/problemsolving. Prerequisite: C or better in ARO 311.
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ARO 312 - Aircraft Jet Propulsion
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ARO 322: L Aerospace Feedback Control Systems/Laboratory
3.00 Credits
California State Polytechnic University-Pomona
Mathematical models of systems. Laplace transformations. Feedback control systems: characteristics, performance, stability. Root locus method. Frequency response methods. Stability in the frequency domain. Time domain analysis. Design and compensation of aerospace feedback control systems. 3 lectures/problemsolving; 1 threehour laboratory. Prerequisites: ENG 104 or IGE 120 or IGE 121 or IGE 122, C or better in MAT 216. Corequisite: MAT 318.
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ARO 322 - L Aerospace Feedback Control Systems/Laboratory
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ARO 326: L Aerospace Structural Mechanics I/Laboratory
3.00 Credits
California State Polytechnic University-Pomona
Vector analysis of twodimensional kinetic motion of aerospace vehicles. Plane kinematics including absolute and relative motion. Force and moment equilibrium in three dimensions using free body diagrams and vector algebra. Internal loads in engine mount, landing gear and fabriccovered wing structures. Shear and bendingmoment diagrams. Centroids, center of gravity, moments of area, and moments of inertia. Material properties, stressstrain relationships, Mohr's circle, strain gages. Analysis of stress in members subject to axial, torsional, bending, and shearing loading. 3 lectures/problemsolving; 1 threehour laboratory. Prerequisites: C or better in PHY 131/L. Corequisite: MAT 214.
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ARO 326 - L Aerospace Structural Mechanics I/Laboratory
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ARO 327: Aerospace Structural Mechanics II
3.00 Credits
California State Polytechnic University-Pomona
External loads on aircraft, inertia forces and load factors, design loads, factor ofand margin ofsafety, Vn diagrams. Strain energy. Analysis of deformation in members subject to axial, torsional, bending, shearing, and combined loading using Castigliano's theorem. Statically indeterminate structures. Pressure vessels, yield criteria. Shear flow in closed and open thinwalled sections. Bending and shear stresses in beams with unsymmetrical crosssections. Principles and analysis of stressed skin construction. 3 lectures/problemsolving. Prerequisite: C or better in ARO 326.
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ARO 327 - Aerospace Structural Mechanics II
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ARO 328: Aerospace Structures
4.00 Credits
California State Polytechnic University-Pomona
Aerospace structural analysis in the design process. Elementary aeroelasticity. Axial constraint. Design of members in tension, torsion, bending, or shear. Design of compression members. Design of webs in shear. Detailed design. 4 lectures/problemsolving. Prerequisite: C or better in ARO 329.
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ARO 329: Aerospace Structural Analysis and Design
3.00 Credits
California State Polytechnic University-Pomona
Work and energy methods. Numerical analysis and introduction to the finite element method. Thin plate theory and structural stability. Elastic and aeroelastic instabilities. Design of Aerospace structures. 3 lectures/problemsolving. Prerequisite: C or better in ARO 327.
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ARO 329 - Aerospace Structural Analysis and Design
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