Initializing Virtual Testing Facility
INDIGO AirGuard
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Flight Dynamics
Test Conditions
Mach
0.000
Reynolds
0.00e0
q (Pa)
0.0
T (K)
288.15
AoA
0.0 deg
Aerodynamic Forces
Lift
0.0 N
Drag
0.0 N
L/D
0.00
CL
0.000
CD
0.000
Structural Analysis
Load Case
Hover (1G)
Peak Stress
0 MPa
Material Yield
800 MPa
Safety Factor
--
Deformation
0.0 mm
Material Properties
Primary
PA-CF / CFRP
E modulus
70 GPa
Density
1550 kg/m3
UTS
800 MPa
Flight Telemetry
Speed
0 km/h
Altitude
0 m AGL
G-Load
1.0 G
Battery
100%
Dist to Target
-- m
Phase
Ready
G-Force
1.0G
0m
ALT
Test Article
Class
A - Wasp
Mass
544 g
Ref. Area
0.053 m2
Wingspan
260 mm
CL vs AoA
CD vs Speed
Drag Polar
L/D vs AoA
Load Cases
Hover (1G)
Max Speed (2G)
Max Maneuver (9G)
Landing Impact (5G)
Stress Distribution
Peak von Mises
0 MPa
Location
--
Safety Factor
--
Material Stack
Skin
CFRP T700
Core
Rohacell 51IG
Mounts
7075-T6 Al
Frame
PA12-CF
Deformation Scale
1x
10x
Mission Scenario
FPV Intercept (Class A)
Patrol Orbit (Class B)
Anti-Shahed (Class C)
High-Speed (Class D)
Mission Status
Elapsed
0.0 s
Speed
0 km/h
Altitude
0 m
G-Load
1.0 G
Battery
100%
Range Used
0 m
Outcome
In Progress
Speed Profile
Altitude Profile
Class
A Wasp
B Hawk
C Falcon
D Eagle
Viz
Streamlines
Pressure
Schlieren
Smoke
Speed
120 km/h
AoA
5.0 deg
Class
A Wasp
B Hawk
C Falcon
D Eagle
View
Stress Map
Deformation
Combined
LAUNCH
RESET
Time Scale
5x
Camera
Chase
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Free