Expert-level aerospace propulsion covering gas turbine engines, rocket propulsion, thermodynamic cycles, nozzle design, and propellant chemistry.
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실행 점수 미검증
설치 방법 보기설치하기 전에 에이전트에게 전달되는 지시 내용을 확인할 수 있습니다.
Turbojet: intake, compressor, combustor, turbine, nozzle. Turbofan: bypass flow around core, better fuel efficiency, lower noise. Bypass ratio: ratio of bypass to core flow, high BPR for subsonic transport. Turboprop: turbine drives propeller via gearbox, efficient at low speed. Compressor pressure ratio: determines thermal efficiency and specific thrust.
Ideal cycle: isentropic compression, constant pressure heat addition, isentropic expansion. Thermal efficiency: eta = 1 minus 1 over r_p to power k-1 over k. Specific fuel consumption: fuel flow per unit thrust, measure of efficiency. Component efficiencies: polytropic efficiency for compressor and turbine. Turbine inlet temperature: key design parameter, limited by material capability.
Rocket equation: delta-V = Isp times g0 times ln m0 over mf. Specific impulse: Isp = thrust over mass flow times g0, measure of propellant efficiency. Liquid propellants: RP-1/LOX, LH2/LOX, hypergolic NTO/MMH. Solid propellants: HTPB-based, simple, reliable, not throttleable. Hybrid: solid fuel with liquid or gaseous oxidizer.
Convergent-divergent nozzle: accelerates flow from subsonic to supersonic. Area ratio: determines exit Mach number and expansion ratio. Nozzle efficiency: accounts for friction and non-uniform flow losses. Thrust coefficient: CF = thrust over P_c times At, measures nozzle performance.
| Pitfall | Fix |
|---|---|
| Ignoring off-design performance | Engine must perform across full flight envelope |
| Overexpanded nozzle at sea level | Check nozzle exit pressure vs ambient |
| Underestimating turbine cooling | TIT limits require significant cooling air fraction |
| Wrong Isp units | Clarify whether Isp is in seconds or N s/kg |
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Expert-level abstract algebra knowledge. Use when working with groups, rings, fields, modules, Galois theory, representation theory, or algebraic structures. Also use when the user mentions 'group', 'ring', 'field', 'homomorphism', 'isomorphism', 'normal subgroup', 'quotient group', 'Sylow theorem', 'Galois theory', 'polynomial ring', 'ideal', 'module', 'vector space', or 'representation theory'.
한국어 요약은 준비 중입니다. 원문 설명을 표시하고 있습니다.
Expert-level acoustics knowledge. Use when working with sound waves, acoustic propagation, resonance, standing waves, Doppler effect, room acoustics, ultrasound, noise control, musical acoustics, or architectural acoustics. Also use when the user mentions 'sound wave', 'decibel', 'frequency', 'resonance', 'standing wave', 'Doppler effect', 'acoustic impedance', 'reverberation', 'ultrasound', 'noise control', 'harmonics', or 'sound intensity'.
한국어 요약은 준비 중입니다. 원문 설명을 표시하고 있습니다.
Expert-level aerodynamics covering subsonic and supersonic flow, lift and drag, airfoil theory, boundary layers, compressible flow, and CFD methods.
한국어 요약은 준비 중입니다. 원문 설명을 표시하고 있습니다.
Expert-level air quality engineering covering pollutant sources, atmospheric dispersion, air quality standards, emission controls, and air quality modeling.
한국어 요약은 준비 중입니다. 원문 설명을 표시하고 있습니다.
Expert-level aircraft structures covering structural design philosophy, wing and fuselage analysis, fatigue and damage tolerance, composite structures, and certification.
한국어 요약은 준비 중입니다. 원문 설명을 표시하고 있습니다.
Expert-level algorithms and complexity theory covering sorting, searching, graph algorithms, dynamic programming, greedy algorithms, NP-completeness, and algorithm design paradigms.
한국어 요약은 준비 중입니다. 원문 설명을 표시하고 있습니다.