Aerospace Engineering (AER E)AEROSPACE ENGINEERING(AER E)Any experimental courses offered by AER E can be found listings/ urses/explistings/)AER E 192: Aerospace SeminarCr. R. S.Vectors, differentiation, integration, matrices, and systems of linearequations.AER E 192H: Aerospace Seminar: Honors.Cr. R. S.Vectors, differentiation, integration, matrices, and systems of linearCourses primarily for undergraduates:equations.AER E 160: Aerospace Engineering Problems With Computer ApplicationsAER E 261: Introduction to Performance and DesignLaboratory(3-0) Cr. 3. F.S.(2-2) Cr. 3. F.S.Prereq: MATH 166, PHYS 221, credit or enrollment in AER E 161Prereq: MATH 143 or satisfactory scores on mathematics placementAerodynamics of the airplane, lift and drag, drag polar, propulsionexaminations; credit or enrollment in MATH 165characteristics of turbojets and piston props, level flight, range,Solving aerospace engineering problems and presenting solutionsendurance, climbing flight, turning flight, take-off and landing, designthrough technical reports. Significant figures and estimation. SI units.examples.Graphing and curve fitting. Introduction to aerospace engineering andengineering design. Spreadsheet programs. History of aerospace.Systems thinking. Team projects.AER E 265: Scientific Balloon Engineering and Operations(Cross-listed with MTEOR). (0-2) Cr. 1. Repeatable. F.Engineering aspects of scientific balloon flights. Integration of scienceAER E 160H: Aerospace Engineering Problems With Computermission objectives with engineering requirements. Operations teamApplications Laboratory: Honorscertification. FAA and FCC regulations, communications, and command(2-2) Cr. 3. F.S.systems. Flight path prediction and control.Prereq: MATH 143 or satisfactory scores on mathematics placementexaminations; credit or enrollment in MATH 165Solving aerospace engineering problems and presenting solutionsthrough technical reports. Significant figures. SI units and estimation.Graphing and curve fitting. Introduction to aerospace engineering andengineering design. Spreadsheet programs. History of aerospace.Systems thinking. Team projects.AER E 161: Numerical, Graphical and Laboratory Techniques forAerospace Engineering(2-2) Cr. 3. F.S.Prereq: Credit or enrollment in AER E 160 or equivalent courseComputer-based problem solving using Matlab(R), with emphasis onnumerical methods. Introduction to solid modeling and aerospace designusing SolidWorks.AER E 161H: Numerical, Graphical and Laboratory Techniques forAerospace Engineering: Honors(2-2) Cr. 3. F.S.Prereq: AER E 160 or equivalent courseComputer-based problem solving using Matlab(R), with emphasis onnumerical methods. Introduction to solid modeling and aerospace designusing SolidWorks.1AER E 290: Aerospace Engineering Independent Study: IndependentStudyCr. 1-2. Repeatable.Prereq: Sophomore classification, approval of the departmentAER E 290A: Aerospace Engineering Independent Study: Flight groundinstructionCr. 1-2. Repeatable.Prereq: Sophomore classification, approval of the departmentAER E 290B: Aerospace Engineering Independent Study: In-flight trainingCr. 1-2. Repeatable.Prereq: AER E 301AER E 290C: Aerospace Engineering Independent Study: OtherCr. 1-2. Repeatable.Prereq: AER E 301
2Aerospace Engineering (AER E)AER E 294: Make to Innovate IAER E 322: Aerospace Structures LaboratoryCr. 1. Repeatable, maximum of 3 credits. F.S.(1-2) Cr. 2. F.S.Prereq: Restricted to Freshman and Sophomore classifications, InstructorPrereq: Credit or enrollment in AER E 321permission required.Design of experiments. Data analysis. Strain gage installation.Multidisciplinary projects to engage students in the fundamentals ofMeasurement of stiffness/strength of aluminum. Analysis/fabrication/engineering, project management, systems engineering, teamwork, andtesting of riveted joints. Shear/bending measurements inbeam sections.oral and visual communication. Students will define and attain their teamAnalysis/measurement of strains in frames. Buckling of columns. Stressobjectives and milestones that are approved by the instructor. Can onlyconcentration. Vibration testing of beams and plates. Fabrication/testingbe used toward graduation in these cases. To make credit deficienciesof composites.in 100 or 200 level courses. No more than 2 credits of Aer E 294X can beused to make-up credit deficiencies in 100 or 200 level courses. Cannotbe used in any category or technical electives in the Aer E curriculumAER E 331: Flight Control Systems I(3-0) Cr. 3. F.S.Prereq: AER E 355AER E 301: Flight ExperienceLinear system analysis. Control system designs using root-locus andCr. R. F.S.frequency response methods. Applications in flight control systems.Prereq: Credit or enrollment in AER E 355Two hours of in-flight training and necessary ground instruction. Coursecontent prescribed by the Aerospace Engineering Department. Ten hoursof flight training certified in a pilot log book can be considered by thecourse instructor as evidence of satisfactory performance in the course.Offered on a satisfactory-fail basis only.AER E 344: Aerodynamics and Propulsion Laboratory(2-2) Cr. 3. F.S.Prereq: AER E 310; Coreq: AER E 311Similitude and dimensional analysis. Measurement uncertainty analysis.Pressure and velocity measurement methods and instruments. Pressuredistribution around a circular cylinder. Aerodynamic performance of low-AER E 310: Aerodynamics I: Incompressible Flowspeed airfoils. Airfoil wake flow; Boundary layer flow. Flow visualization(3-0) Cr. 3. F.S.techniques for supersonic flows and de Laval nozzles.Prereq: Grade of C- or better in AER E 261 and MATH 265Introduction to fluid mechanics and aerodynamics. Fluid propertiesand kinematics. Conservation equations in differential and integralform. Bernoulli's equation. Basic potential flow concepts and solutions.Boundary layer concept. Incompressible flow over airfoils and wings.Examples of numerical methods. Applications of multi-variable calculusto fluid mechanics and aerodynamics.AER E 311: Aerodynamics II: Compressible Flow(3-0) Cr. 3. F.S.Prereq: AER E 310, M E 231Review of thermodynamics, energy equation, compressible flow, andisentropic flow. Normal and oblique shocks. Mach waves and expansionfans. Applications to ducts and nozzles. Compressible airfoil and wingtheory. Introduction to advanced compressible flow topics.AER E 321: Flight Structures Analysis(3-0) Cr. 3. F.S.Prereq: E M 324, Credit or enrollment in MATH 266 or 267Introduction to elasticity, airworthiness, and flight loads. Introductionto fatigue. Materials selection for flight applications. Thin walledcross-sections under bending, torsion, and shear loads using classicalmethods. Shear center. Column buckling. Matrix methods of structuralanalysis.AER E 351: Astrodynamics I(3-0) Cr. 3. F.S.Prereq: M E 345Introduction to astrodynamics. Two-body Keplerian satellite andplanetary motion. Geocentric and extraterrestrial trajectories andapplications. Ballistic missiles.AER E 355: Aircraft Flight Dynamics and Control(3-0) Cr. 3. F.S.Prereq: AER E 261, MATH 267, M E 345Aircraft rigid body equations of motion, linearization, and modal analysis.Longitudinal and lateral-directional static and dynamic stability analysis.Flight handling characteristics analysis. Longitudinal and lateraldirectional open loop response to aircraft control inputs. Aircraft flighthandling qualities.AER E 361: Computational Techniques for Aerospace Design(2-2) Cr. 3. F.S.Prereq: AER E 310, MATH 267, E M 324, M E 345Advanced programming, workstation environment, and development ofcomputational tools for aerospace analysis and design. Technical reportwriting.
Aerospace Engineering (AER E)3AER E 362: Aerospace Systems IntegrationAER E 407: Applied Formal Methods(3-0) Cr. 3. F.S.(Dual-listed with AER E 507). (Cross-listed with COM S). Cr. 3. S.Prereq: ENGL 250, Junior standing in Aerospace Engineering or permission ofPrereq: AER E 361 for AER E majors. COM S 311 for COM S majors. AER E 361instructoror COM S 311, or an equivalent course, plus instructor permission for otherEmphasis on impact of component interfaces in aerospace systems.majors.Understand how changes in variables associated with individualIntroduction to the fundamentals of formal methods, a set ofcomponents impact the performance of the aerospace system. Solvingmathematically rigorous techniques for the formal specification,aerospace engineering problems and presenting solutions throughvalidation, and verification of safety- and security-critical systems. Tools,reports. Specific integration challenges include: capturing implicittechniques, and applications of formal methods with an emphasis ondisciplinary interactions (e.g. structures/aerodynamics, propulsion/real-world use-cases such as enabling autonomous operation. Buildaerodynamics, etc.), propagating tolerances through the system (i.e.experience in writing mathematically analyzable specifications fromuncertainty modeling), balancing component attributes in the systemEnglish operational concepts for real cyberphysical systems, such asobjective.aircraft and spacecraft. Review capabilities and limitations of formalAER E 381: Introduction to Wind Energy(3-0) Cr. 3. S.methods in the design, verification, and system health management oftoday's complex systems.Prereq: MATH 166, PHYS 221AER E 411: Aerospace Vehicle PropulsionBasic introduction to the fundamentals of Wind Energy and Wind Energy(3-0) Cr. 3. F.S.conversion systems. Topics include but not limited to various types ofPrereq: AER E 311, AER E 344wind energy conversion systems and the aerodynamics, blade and towerAtmospheric propulsion system performance and cycle analysis.structural loads, kinematics of the blades and meteorology.Momentum theorem, thrust and propulsive efficiency. ThermodynamicsAER E 396: Summer InternshipCr. R. Repeatable. SS.Prereq: Permission of department and Engineering Career Servicesof compressible flow with heat and work addition. Components andprinciples of turbojet, ramjet, and turbofan aircraft engines. Introductionto rocket engines.Professional work period of at least 10 weeks during the summer.AER E 412: Spacecraft Electric PropulsionStudents must register for this course prior to commencing work. Offered(3-0) Cr. 3. S.on a satisfactory-fail basis only.Prereq: AER E 311AER E 398: Cooperative EducationCr. R. Repeatable. F.S.Prereq: Permission of department and Engineering Career Services.Electricity and magnetism. Plasma physics. Ion engine performance.Introduction to advanced electromagnetic propulsion systems. Energysources and nuclear propulsion. Space mission requirements.Professional work period. One semester per academic or calendar year.AER E 415: Rocket PropulsionStudents must register for this course prior to commencing work. Offered(3-0) Cr. 3. F.S.on a satisfactory-fail basis only.Prereq: AER E 311 and AER E 344Components and principles of liquid rocket engines, solid rocketmotors, and hybrid rocket motors. Rocket flight performance and rocketstaging. Combustion and thermochemistry. Rocket cooling and nozzleheat transfer. Introduction to nuclear thermal propulsion and electricpropulsion systems. Applications to spacecraft.
4Aerospace Engineering (AER E)AER E 417: Experimental MechanicsAER E 432: Flight Control Systems II(Dual-listed with AER E 517). (Cross-listed with E M). (2-2) Cr. 3. Alt. F.,(3-0) Cr. 3. F.offered even-numbered years.Prereq: AER E 331Prereq: E M 324; MAT E 273Aircraft lateral directional stability augmentation. Launch vehicleIntroduction to fundamental concepts for force, displacement, stresspitch control system design. Control of flexible vehicles. Satelliteand strain measurements for structures and materials applications.attitude control. Flight control designs based on state-space methods.Strain gage theory and application. Full field deformation measurementsIntroduction to sample-data systems.with laser interferometry and digital image processing. Advancedexperimental concepts at the micro- and nano-scale regimes. Selectedlaboratory experiments.AER E 433: Spacecraft Dynamics and Control(3-0) Cr. 3. F.Prereq: M E 345AER E 421: Advanced Flight StructuresThree-dimensional rotational kinematics and attitude dynamics of a rigid(2-2) Cr. 3. F.S.body in space. Classical stability analysis of spinning spacecraft with orPrereq: AER E 321, MATH 266 or MATH 267without energy dissipation. Attitude dynamics, stability, and control ofAnalysis of indeterminate flight structures including finite elementspacecraft in a circular orbit in the presence of gravity-gradient torques.laboratory. Static analysis of complex structural components subject toIntroduction to spacecraft attitude determination and control systemsthermal and aerodynamic loads. Analytical and finite element solutions(ADCS) with emphasis on modern attitude determination algorithms.for stresses and displacements of membrane, plane stress, plateSimulation of spacecraft attitude dynamics and control problems ofstructures. Buckling of beams, frames, and plate structures. Introductionpractical interest using programming and analysis software.to vibration of flight structures. Steady state and transient structuralresponse using normal modal analysis.AER E 442: V/STOL Aerodynamics and Performance(3-0) Cr. 3. F.AER E 422: Vibrations and AeroelasticityPrereq: AER E 261(3-0) Cr. 3. Alt. S., offered even-numbered years.Introduction to the aerodynamics, performance, stability, control andPrereq: E M 324 or AER E 321critical maneuvering characteristics of V/STOL vehicles. Topics includeVibration theory. Steady and unsteady flows. Mathematical foundationshovercrafts, jet flaps, ducted fans and thrust vectored engines.of aeroelasticity, static and dynamic aeroelasticity. Linear unsteadyaerodynamics, non-steady aerodynamics of lifting surfaces. Stall flutter.Aeroelastic problems in civil engineering structures. Aeroelastic problemsof rotorcraft. Experimental aeroelasticity. Selected wind tunnel laboratoryexperiments.AER E 445: Experimental Flow Mechanics and Heat Transfer(Dual-listed with AER E 545). (3-0) Cr. 3. F.Prereq: AER E 310 or M E 335 or A B E 378Similitude and dimensional analysis. Measurement uncertaintyanalysis; Fluid mechanical apparatus: wind tunnel and water tunnels.AER E 423: Composite Flight StructuresVarious experimental techniques widely used for fluid mechanics,(2-2) Cr. 3. S.aerodynamics, heat transfer, and combustion studies: Pressure gaugePrereq: E M 324; MAT E 273and transducers; Pitot tube; hot wire anemometry; Shadowgraph andFabrication, testing and analysis of composite materials used inSchlieren Photography; laser Doppler velocimetry; particle imageflight structures. Basic laminate theory of beams, plates and shells.velocimetry (PIV); advanced PIV techniques (stereo PIV, 3-D PIV,Manufacturing and machining considerations of various types ofTomographic PIV, Holograph PIV and microscopic PIV); laser inducedcomposites. Testing of composites for material properties, strength andfluorescence; pressure sensitive painting, temperature sensitive painting;defects. Student projects required.molecular tagging velocimetry; molecular tagging thermometry. ExtensiveAER E 426: Design of Aerospace Structures(Dual-listed with AER E 526). (2-2) Cr. 3. F.Prereq: E M 324Detailed design and analysis of aerospace vehicle structures. Materialselection, strength, durability and damage tolerance, and validationanalysis. Design for manufacturability.applications and laboratory experiments will be included.
Aerospace Engineering (AER E)AER E 446: Computational Fluid DynamicsAER E 462: Design of Aerospace Systems(3-0) Cr. 3. F.(1-4) Cr. 3. F.S.Prereq: AER E 311, AER E 361 and proficiency in at least one programmingPrereq: AER E 461languageFundamental principles used in engineering design of aircraft, rockets,Introduction to computational fluid dynamics. Discretization, consistency,and space systems. Preliminary design of aerospace vehicles.and stability. Explicit and implicit methods for ordinary and partialEngineering Ethics. The class contains two focus sections. One sectiondifferential equations. Linearization techniques. Iterative and directassigns design projects in Aeronautics, and the other section assignssolution algorithms. Numerical methods for parabolic, elliptic anddesign projects in Astronautics.hyperbolic equations. Curvilinear coordinates and numerical gridgeneration. Applications to Euler, boundary-layer and Navier-Stokesequations.AER E 463: Introduction to Multidisciplinary Design Optimization(Dual-listed with AER E 563). (3-0) Cr. 3. F.Prereq: senior standing in College of Engineering or permission of instructorAER E 448: Fluid Dynamics of TurbomachineryIntroduction to the theory and methods of Multidisciplinary Design(Cross-listed with M E). (3-0) Cr. 3. S.Optimization (MDO), including system coupling, system sensitivityPrereq: AER E 311 or M E 335methods, decomposition methods, MDO formulations (such as multi-Applications of principles of fluid mechanics and thermodynamics indiscipline feasible (MDF), individual discipline feasible (IDF) and all-at-performance analysis and design of turbomachines. Conceptual andonce (AAO) approaches, and MDO search methods.preliminary design of axial and radial flow compressors and turbinesusing velocity triangles and through-flow approaches.AER E 464: Spacecraft Systems(3-0) Cr. 3. S.AER E 451: Astrodynamics IIPrereq: AER E 351(3-0) Cr. 3. F.S.An examination of spacecraft systems including attitude determinationPrereq: AER E 351and control, power, thermal control, communications, propulsion,Orbit determination and prediction using Gibb's and Gauss' methods.guidance, navigation, command and data handling, and mechanisms.Advanced orbit maneuvers, triple-, and fixed-impulse; universal variables;Explanation of space and operational environments as they impactKepler's problem. Earth gravity field models and gravity harmonics, orbitspacecraft design. Includes discussion of safety, reliability, quality,perturbations, advanced dynamics, variational methods, relative orbitalmaintainability, testing, cost, legal, and logistics issues.mechanics, and Clohessy-Wiltshire equations.5AER E 466: Multidisciplinary Engineering DesignAER E 452: Introduction To Systems Engineering And Analysis(Cross-listed with A B E, B M E, CPR E, E E, ENGR, I E, M E, MAT E). (1-4) Cr.(Cross-listed with I E). Cr. 3. SS.3. Repeatable. F.S.Prereq: Junior Classification in an Engineering MajorPrereq: Student must be within two semesters of graduation; permission ofPrinciples of systems engineering to include problem statementinstructor.formulation, stakeholder analysis, requirements definition, systemApplication of team design concepts to projects of a multidisciplinaryarchitecture and concept generation, system integration and interfacenature. Concurrent treatment of design, manufacturing, and life cyclemanagement, verification and validation, and system commissioning andconsiderations. Application of design tools such as CAD, CAM, anddecommissioning operations. Introduction to discrete event simulationFEM. Design methodologies, project scheduling, cost estimating,processes. Students will work in groups to propose, research, and presentquality control, manufacturing processes. Development of a prototypefindings for a systems engineering topic of current relevance.and appropriate documentation in the form of written reports, oralAER E 461: Modern Design Methodology with Aerospace Applications(2-2) Cr. 3. F.S.Prereq: AER E 361, AER E 311, AER E 321, AER E 322, AER E 344, AER E 351,AER E 355Introduction to modern engineering design methodology. Computationalconstrained optimal design approach including selection of objectivefunction, characterization of constraint system, materials and strengthconsiderations, and sensitivity analyses. The class contains two focussections. One section assigns desi
Vibration theory. Steady and unsteady flows. Mathematical foundations of aeroelasticity, static and dynamic aeroelasticity. Linear unsteady aerodynamics, non-steady aerodynamics of lifting surfaces. Stall flutter. Aeroelastic problems in civil engineering structures. Aeroelastic problems of
Aerospace Engineering 2 *Technical electives can be chosen from the following list. At least three credit hours must come from either AER/ME 501 OR AER/ME 590. AER 380 Topics in Aerospace Engineering (Variable Topics) AER/ME 530 Gas Dynamics AER/ME 531 Fluid Dynamics I AER/ME 532 Advanced Strength of Materials AER 545 Aircraft Control and .
Active Duty AER Request Packet Army Community Service (ACS) Army Emergency Relief (AER) TEL: (719) 526-4590 Use the two part checklist below to prepare AER requests. You can also contact your unit Command Financial NCO (CFNCO), 1SG or Commander; all can assist. Attach copies of supporting documents; do not attach originals. Requests
Grade Level/4-H Experince Pre-Flight (1) Aerospace Lift-Off (2) Aerospace Reaching New Heigts (3) Aerospace Pilot in Command (4) Aerospace Flight Crew Aerospace Leaders Launching Youth Aerospace Programs Aerospace Leaders Gifts of Gold: Seeds, Stalks, & Science Agriculture Gifts of Gold: Food
AAEF2-025: Dressing aircraft engines (Aerospace and Aviation) AAEF2-017: Maintaining mechanical devices and equipment (Aerospace and Aviation) AAEF2-026: Maintaining aircraft mechanical devices and equipment (Aerospace and Aviation) AAEF2-024: General electrical and electronic engineering applications (Aerospace and Aviation)
Aerospace Retirees’ Club (- Name of Board Member -) P.O. Box 2194 El Segundo, CA 90245 Call the ARC voicemail: 310-336-5454, Box 12582 NOTICE The expressions of opinion in the Aerospace Retirees’ Club Newsletter are the opinions of the writers and not necessarily those of the Aerospace Retirees’ Club or The Aerospace Corporation.
AS9100 Aerospace Standard, SAE AS9131 Aerospace Standard, SAE, Nonconformance Documentation AQMSM1001 Aerospace Quality Management System Manual, Kavlico AP0410 Aerospace Procedure for Receiving Inspection AP0410-1 Aerospace Procedure for In-Process Inspection AP0410-2
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oilfield waste generator or oilfield waste receiver. Each AER requirement that is unique to this directive is numbered. Information on compliance and enforcement can be found on the AER website. 1) All documentation required under this directive must be provided to the AER upon request to confirm compliance.