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Mass at Nose 0.0 Grams Throwing Velocity 20.0 KM/HR Stabilizer Incidence Angle 4.9 Degrees

The document contains plans and specifications for an aery glider. It lists dimensions for the fuselage, wing, horizontal stabilizer, and vertical stabilizer. Key specifications include a mass of 39.42 grams, wing loading of 0.103 g/cm^2, and a throwing velocity of 20 km/hr. Performance estimates indicate it will stall at 13.87 km/hr and have a glide angle of 3.94 degrees.

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Quinn Lynch
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73 views4 pages

Mass at Nose 0.0 Grams Throwing Velocity 20.0 KM/HR Stabilizer Incidence Angle 4.9 Degrees

The document contains plans and specifications for an aery glider. It lists dimensions for the fuselage, wing, horizontal stabilizer, and vertical stabilizer. Key specifications include a mass of 39.42 grams, wing loading of 0.103 g/cm^2, and a throwing velocity of 20 km/hr. Performance estimates indicate it will stall at 13.87 km/hr and have a glide angle of 3.94 degrees.

Uploaded by

Quinn Lynch
Copyright
© © All Rights Reserved
We take content rights seriously. If you suspect this is your content, claim it here.
Available Formats
Download as PDF, TXT or read online on Scribd
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Aery Fuselage Plans

Mass at Nose = 0.0 grams


Throwing Velocity = 20.0 km/hr
Stabilizer Incidence Angle = 4.9 degrees

47.5 cm 38.5 cm

Front

14.8 cm

55.1 cm

canard: Page 1
Aery Wing and Horizontal Stabilizer Plans
(Wing & H.S. are not drawn to the same scale)
Front
7.7 cm

2.0 cm

50.3 cm 19.2 cm
Wing Stab.

7.6 cm 5.5 cm

5.5 cm

7.6 cm
canard: Page 2
Aery Vertical Stabilizer Plans

Front

3.2 cm
7.6 cm

13.6 cm

4.90 deg. angle for h.s.


7.6 cm

Data

Filename: luftwaffle part 2 electric boogaloo canard.ae

Configuration:

Center of Gravity = 35.7 cm

Neutral Point = 39.7 cm

Wing Loading = 0.103 g/cm^2

canard: Page 3
Aery Glider Information

It will fly!

The stabilizer may be larger than necessary.

Dimensions & Statistics


Aery Evaluation Number: 132
Fuselage Length: 55.10 cm
Wing Location: 38.46 cm
Stabilizer Location: 14.78 cm
Vertical Tail Location: 47.48 cm
Mass at Nose: 0.00 g

Center of Gravity Location: 35.67 cm


Neutral Point Location: 39.65 cm
ESTIMATED Mass: 39.42 g
Wing Loading 0.103 g/cm^2

Throwing Velocity: 20.00 km/hr


Flight Angle of Attack: 4.67 degrees
Stabilizer Incidence Angle: 4.90 degrees (positive upward)
ESTIMATED Stall Angle: 10.98 degrees
ESTIMATED Stall Velocity: 13.87 km/hr
ESTIMATED Glide Angle: 3.94 degrees (positive downward)
ESTIMATED CDo: 0.020

Wing Span: 50.29 cm


Planform Area 383.23 cm^2
Wing Root Chord: 7.62 cm
Wing Taper Ratio: 1.00
Wing Tip Chord: 7.62 cm
Wing Tip Sweep Distance: 7.69 cm
Wing Leading Edge Sweep Angle: 17.00 degrees
Wing Aspect Ratio: 6.60
CL,alpha: 4.50 1/radian

Stabilizer Span: 19.22 cm


Planform Area 105.90 cm^2
Stabilizer Root Chord: 5.51 cm
Stabilizer Taper Ratio: 1.00
Stabilizer Tip Chord: 5.51 cm
Stabilizer Tip Sweep Distance: 1.98 cm
Stabilizer Leading Edge Sweep Angle: 11.62 degrees
Stabilizer Aspect Ratio: 3.49
CL,alpha: 3.66 1/radian

Vertical Tail Height: 13.63 cm


Planform Area 103.86 cm^2
Vertical Tail Root Chord: 7.62 cm
Vertical Tail Taper Ratio: 1.00
Vertical Tail Tip Chord: 7.62 cm
Vertical Tail Tip Sweep Distance: 3.17 cm
Vertical Tail Leading Edge Sweep Angle: 13.10 degrees

canard: Page 4

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