Aerodynamics
Four forces, angle of attack, lift and drag, stability, load factor, and performance relationships.
A professional quick-reference library for flight, aerospace engineering, avionics, navigation, weather, propulsion, aircraft systems, unmanned systems, and spaceflight terminology.
Start with a term, jump to a technical topic, or use the quick-reference panels while working through aerospace lessons and simulator training.
Four forces, angle of attack, lift and drag, stability, load factor, and performance relationships.
PFD, MFD, GTC, flight director, autopilot, navigation displays, engine information, and scan priorities.
Heading, course, track, GPS/GNSS, VOR, RNAV, ILS, airport references, and common navigation abbreviations.
METAR, TAF, wind, visibility, pressure, temperature, clouds, turbulence, and weather information sources.
Piston-engine and propeller fundamentals, RPM, manifold pressure, temperatures, thrust, and efficiency.
Flight controls, electrical, fuel, landing gear, braking, environmental, safety, and structural systems.
UAS terminology, FAA TRUST, command and control, situational awareness, and system-level thinking.
Orbit families, spacecraft attitude control, communications, guidance, propulsion, and mission architecture.
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Core relationships students should recognize when analyzing aircraft behavior and performance.
| Force | Direction | Primary Idea |
|---|---|---|
| Lift | Perpendicular to relative wind | Aerodynamic force generated primarily by the wings. |
| Weight | Toward Earth | Gravitational force acting through the center of gravity. |
| Thrust | Generally forward | Propulsive force produced by the engine/propeller or other propulsion system. |
| Drag | Opposes relative motion | Aerodynamic resistance to movement through the air. |
The standard engineering form of the lift equation helps explain why airspeed, air density, wing area, and lift coefficient matter.
Angle of attack (AOA) is the angle between the airfoil chord line and the relative wind. It is not the same as pitch attitude.
Use this section with the Cirrus G7 simulator and other integrated flight-deck lessons.
Automation should reduce workload without reducing awareness. Before selecting a mode, identify the desired aircraft behavior, select the control, then verify the mode annunciation and aircraft response.
| METAR | Observed weather at an aerodrome. |
| TAF | Forecast weather for a terminal area. |
| ATIS | Recorded terminal information including weather and runway details. |
| AWOS / ASOS | Automated surface weather observations. |
| NOTAM | Time-sensitive operational information that may affect a flight. |
Wind is described by the direction from which it is blowing. A runway aligned more closely with the wind reduces the crosswind component.
Air density changes with pressure, temperature, and altitude. Lower density generally reduces aerodynamic and engine/propeller performance.
A propeller is a rotating airfoil. Blade angle, rotational speed, forward speed, air density, and engine power all affect thrust and efficiency.
Gas-turbine engines compress incoming air, add energy through combustion, and accelerate the flow through the turbine/nozzle system. Thrust follows from the change in momentum of the airflow.
Rocket engines carry both fuel and oxidizer, allowing operation without atmospheric oxygen. Thrust is produced by accelerating exhaust mass through the nozzle.
Ailerons control roll, elevator/stabilator controls pitch, and rudder controls yaw.
Flaps, trim, spoilers, and other devices modify lift, drag, control force, or configuration.
Battery, alternator/generator, buses, circuit protection, loads, and emergency/essential power architecture.
Storage, venting, selection, delivery, quantity indication, pumps, and engine-feed architecture.
Fuselage, wing, empennage, control surfaces, landing gear, load paths, and structural design tradeoffs.
Ground support, steering, braking, shock absorption, and energy dissipation during landing and taxi.
Pressure sources used to support airspeed, altitude, and vertical-speed indications.
ELT and aircraft-specific emergency equipment, checklists, redundancy, and system isolation concepts.
| LEO | Low Earth Orbit; used by many crewed spacecraft, imaging satellites, and large constellations. |
| MEO | Medium Earth Orbit; includes important navigation-satellite regimes. |
| GEO | Geostationary Earth Orbit; equatorial orbit matching Earth's rotation period. |
| Polar | High-inclination orbit that passes near the poles and can provide broad Earth coverage over time. |
Attitude describes spacecraft orientation. Orbit describes its trajectory around a body. Reaction wheels, control moment gyros, magnetic torquers, and thrusters are examples of attitude-control technologies.
Professional aerospace design treats a mission as an integrated system: requirements, launch, spacecraft, ground segment, communications, operations, payload, risk, cost, and verification all interact.
Use these authoritative sources when a class assignment requires deeper technical detail or current operational information.
Educational reference: This page is designed for classroom learning and simulator study. It does not replace current FAA publications, aircraft-specific manuals, instructor guidance, or required operational checklists.
Use the searchable glossary above online, or print this page when you need a paper reference during class. The glossary is intentionally written in short technical language so it works as both a study tool and a desk reference.