Αεροδιαστημική Μηχανολογία Jobs

The assignment involves analysing and designing a propeller propulsion system for a Bristell NG-5 aircraft. There are three main tasks: Propeller Design: Use Blade Element Momentum Theory (BEMT) to calculate propeller performance, using real aerofoil data, and conduct sensitivity analysis and experimental validation. Engine Analysis: Perform thermodynamic calculations to determine engine power and fuel consumption (BSFC) at sea level and different altitudes, and compare results with existing aircraft engines. Engine–Propeller Matching: Determine the optimal propeller diameter, number of blades, blade pitch distribution, and RPM settings for climbing and cruising while minimising fuel consumption. Required deliverables: A professional engineering report (maximum 8 pages, excludi...

Sabit kanatlı, mini sınıfta bir İHA tasarlamak istiyorum. Platform gözetleme amacıyla kullanılacak; dolayısıyla dengeli aerodinamik yapı, düşük gürültü izi ve istikrarlı uçuş performansı kritik. Beklediğim ana teslimatlar • Aerodinamik konsept çalışması ve 3-görünüş çizimi • Yapısal tasarım (malzeme seçimi, ağırlık dağılımı, kabuk–iskelet detayı) • Gövde, kanat ve kuyruk için CAD modelleri (SolidWorks veya benzeri) • Uçuş performans hesapları (menzil, havada kalma, azami hız) • Elektrik-elektronik yerleşim diyagramı (otopilot, sensör, batarya, anten) • Parça listesi ve üretim/entegrasyon rehberi İhtiyaçlar • Tasarımın ger&c...

I’m developing an aerodynamic housing for an aerospace application and need the outer shell replicated from the reference images I will supply. The form is a fluid, complex blend of curves roughly 1200 × 900 × 250–300 mm; exact dimensions may shift as long as the visual intent is preserved. Only the external body is required—no internals, ribs, or mounting details yet—so every effort can focus on Class-A surface quality and crisp symmetry. Your task is to create the part natively in SolidWorks, modelling with surface tools (lofts, boundary, fill, etc.) until tangency and curvature continuity are clean throughout. I must receive a fully editable .SLDPRT file; neutral formats like STEP/IGES can come along for convenience but are not a substitute. Deliver...

I’m developing an aerodynamic housing for an aerospace application and need the outer shell replicated from the reference images I will supply. The form is a fluid, complex blend of curves roughly 1200 × 900 × 250–300 mm; exact dimensions may shift as long as the visual intent is preserved. Only the external body is required—no internals, ribs, or mounting details yet—so every effort can focus on Class-A surface quality and crisp symmetry. Your task is to create the part natively in SolidWorks, modelling with surface tools (lofts, boundary, fill, etc.) until tangency and curvature continuity are clean throughout. I must receive a fully editable .SLDPRT file; neutral formats like STEP/IGES can come along for convenience but are not a substitute. Deliver...