I offer comprehensive aircraft & UAV preliminary design
About this service
I provide preliminary aircraft and UAV design from mission requirements, taking the project from initial requirements to a technically justified aircraft configuration.
You will receive:
✅ Mission requirement breakdown and design objectives
✅ MTOW and preliminary weight breakdown
✅ Engine (Propulsion) selection, Wing loading, thrust/power loading and sizing
✅ Wing area, span, aspect ratio and taper selection
✅ Airfoil and aerodynamic configuration selection
✅ Cruise, stall, climb and maximum-speed estimation
✅ Range and endurance estimation
✅ Propulsion requirement and preliminary selection
✅ Constraint analysis and design-point selection
✅ Initial CG, stability and control considerations
✅ Configuration trade studies and design comparison
✅ Preliminary aircraft specifications and engineering recommendations
You will receive:
✅ Mission requirement breakdown and design objectives
✅ MTOW and preliminary weight breakdown
✅ Engine (Propulsion) selection, Wing loading, thrust/power loading and sizing
✅ Wing area, span, aspect ratio and taper selection
✅ Airfoil and aerodynamic configuration selection
✅ Cruise, stall, climb and maximum-speed estimation
✅ Range and endurance estimation
✅ Propulsion requirement and preliminary selection
✅ Constraint analysis and design-point selection
✅ Initial CG, stability and control considerations
✅ Configuration trade studies and design comparison
✅ Preliminary aircraft specifications and engineering recommendations
I provide preliminary aircraft and UAV design from mission requirements, taking the project from initial requirements to a technically justified aircraft configuration.
You will receive:
✅ Mission requirement breakdown and design objectives
✅ MTOW and preliminary weight breakdown
✅ Engine (Propulsion) selection, Wing loading, thrust/power loading and sizing
✅ Wing area, span, aspect ratio and taper selection
✅ Airfoil and aerodynamic configuration selection
✅ Cruise, stall, climb and maximum-speed estimation
✅ Range and endurance estimation
✅ Propulsion requirement and preliminary selection
✅ Constraint analysis and design-point selection
✅ Initial CG, stability and control considerations
✅ Configuration trade studies and design comparison
✅ Preliminary aircraft specifications and engineering recommendations
You will receive:
✅ Mission requirement breakdown and design objectives
✅ MTOW and preliminary weight breakdown
✅ Engine (Propulsion) selection, Wing loading, thrust/power loading and sizing
✅ Wing area, span, aspect ratio and taper selection
✅ Airfoil and aerodynamic configuration selection
✅ Cruise, stall, climb and maximum-speed estimation
✅ Range and endurance estimation
✅ Propulsion requirement and preliminary selection
✅ Constraint analysis and design-point selection
✅ Initial CG, stability and control considerations
✅ Configuration trade studies and design comparison
✅ Preliminary aircraft specifications and engineering recommendations
I provide preliminary aircraft and UAV design from mission requirements, taking the project from initial requirements to a technically justified aircraft configuration.
You will receive:
✅ Mission requirement breakdown and design objectives
✅ MTOW and preliminary weight breakdown
✅ Engine (Propulsion) selection, Wing loading, thrust/power loading and sizing
✅ Wing area, span, aspect ratio and... read more
You will receive:
✅ Mission requirement breakdown and design objectives
✅ MTOW and preliminary weight breakdown
✅ Engine (Propulsion) selection, Wing loading, thrust/power loading and sizing
✅ Wing area, span, aspect ratio and... read more
I provide preliminary aircraft and UAV design from mission requirements, taking the project from initial requirements to a technically justified aircraft configuration.
You will receive:
✅ Mission requirement breakdown and design objectives
✅ MTOW and preliminary weight breakdown
✅ Engine (Propulsion) selection, Wing loading, thrust/power loading and sizing
✅ Wing area, span, aspect ratio and taper selection
✅ Airfoil and aerodynamic configuration selection
✅ Cruise, stall, climb and maximum-speed estimation
✅ Range and endurance estimation
✅ Propulsion requirement and preliminary selection
✅ Constraint analysis and design-point selection
✅ Initial CG, stability and control considerations
✅ Configuration trade studies and design comparison
✅ Preliminary aircraft specifications and engineering recommendations read less
You will receive:
✅ Mission requirement breakdown and design objectives
✅ MTOW and preliminary weight breakdown
✅ Engine (Propulsion) selection, Wing loading, thrust/power loading and sizing
✅ Wing area, span, aspect ratio and taper selection
✅ Airfoil and aerodynamic configuration selection
✅ Cruise, stall, climb and maximum-speed estimation
✅ Range and endurance estimation
✅ Propulsion requirement and preliminary selection
✅ Constraint analysis and design-point selection
✅ Initial CG, stability and control considerations
✅ Configuration trade studies and design comparison
✅ Preliminary aircraft specifications and engineering recommendations read less
Service offer categories
Aerospace Engineering
Machine Design
Mechanical Engineering
Software & skills
Aerodynamic Analysis
Aerodynamic Design
Aerospace Design
Aircraft Design
Aircraft Performance
Aircraft Structure Design
Ansys Simulation
Engineering Analysis
Fixed-wing aircraft
NASA OpenVSP
+7 more
Member since
August 2026
Languages
English
Avg. response time
1 hour
Aerospace & Mechanical Engineer | CFD | FEA | UAV Design
I am an Aerospace & Mechanical Engineer specializing in CFD, FEA, thermal analysis, aerodynamics, UAV design, and engineering simulation.
I provide engineering analysis and design support to startups, OEMs, researchers, and product-development teams.
CFD: Internal & External Flow, Turbulence, Mixing, Multiphase Flow, DPM/Particle Tracking, Pressure Drop, Flow Distribution, Air Purification, HVAC... read more
I provide engineering analysis and design support to startups, OEMs, researchers, and product-development teams.
CFD: Internal & External Flow, Turbulence, Mixing, Multiphase Flow, DPM/Particle Tracking, Pressure Drop, Flow Distribution, Air Purification, HVAC... read more
Questions and answers
Yes. I can start from requirements such as payload, range, endurance, speed, altitude and launch/recovery method and develop a preliminary aircraft configuration and performance estimate.
Yes. I can use your existing configuration as a baseline, calculate its expected performance and identify sizing, aerodynamic or propulsion changes required to meet the mission requirements.
The work can include preliminary configuration development, including wing, tail, fuselage and propulsion architecture, supported by sizing and performance calculations.
We can support the complete development cycle. Our dedicated hardware team can handle detailed CAD, structures, prototyping, testing and production development, while our software/aerodynamics team can take the design from preliminary sizing through detailed engineering, including avionics with production-ready design.
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