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Project Gallery

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Project Gallery

Explore curated aircraft designs analyzed with AeroForge. Load any project into the workspace to study its aerodynamics, or use one as a starting point for your own design.

8 projects
FEATURED
SAILPLANE

ASW 28 Sailplane Study

High-aspect-ratio sailplane analysis. Showcases the importance of minimizing induced drag and achieving L/D > 40 for cross-country soaring performance.

Airfoil
Wortmann FX 61-163
Span
15 m
Max L/D
43.0
Stability
Stable
sailplanehigh ARsoaring
by AeroForge Team
FEATURED
GENERAL AVIATION

Cessna 172 Baseline

A full aerodynamic study of the Cessna 172 Skyhawk, the most-produced aircraft in history. NACA 2412 airfoil, tricycle gear, conventional tail. Great starting point for GA analysis.

Airfoil
NACA 2412
Span
11 m
Max L/D
12.8
Stability
Stable
GAtrainerbaseline
by AeroForge Team
FEATURED
EXPERIMENTAL

Long-EZ Canard

Burt Rutan's famous canard pusher. Demonstrates how AeroForge handles unconventional configurations with forward lifting surface and aft wing.

Airfoil
Eppler 1230
Span
7.92 m
Max L/D
18.2
Stability
Stable
canardexperimentalcomposite
by Community
FEATURED
COMMERCIAL TRANSPORT

Twin Turboprop Transport

A twin-engine turboprop regional transport in the 50-seat class. Demonstrates multi-engine weight & balance, high-wing stability, and cruise optimization.

Airfoil
NASA SC(2)-0714
Span
27.1 m
Max L/D
16.4
Stability
Stable
transportturbopropregional
by AeroForge Team
CONCEPT

Blended Wing Body Concept

A next-generation blended wing body layout. Explores unconventional planforms where the fuselage contributes significant lift. High L/D but challenging stability.

Airfoil
NACA 23015
Span
42 m
Max L/D
22.0
Stability
Unstable
BWBconcepthigh efficiency
by Community
FIGHTER

F-16 Configuration Study

Simplified F-16 Falcon geometry for exploring high-alpha, strake vortex, and relaxed static stability concepts. Uses NACA 64A-204.

Airfoil
NACA 64A-204
Span
10 m
Max L/D
9.2
Stability
Unstable
fightermilitaryhigh-alpha
by Community
UAV

Solar High-Altitude UAV

Ultra-high-aspect-ratio solar-powered UAV concept. Designed for loitering at 18,000 ft with minimal power. Demonstrates extreme AR and low speed analysis.

Airfoil
DAE 11
Span
25 m
Max L/D
35.0
Stability
Stable
solarHALEendurance
by Community
UAV

Swept Flying Wing (RC)

A 1.2m swept flying wing for FPV. Shows low-Re analysis at Re = 200,000 and reflexed airfoil for tailless stability.

Airfoil
MH 45
Span
1.2 m
Max L/D
14.5
Stability
Stable
RCFPVflying wing
by Community