early tailplane - scale soaring uk · pdf filenaca2412 naca2416 late wing early wing aileron...

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Skid contains 12 tennis Balls as part of the suspension 1936 Minimum sinking velocity - 2.5 ft./sec. at 38 m.p.h. Maximum gliding angle - Approx. 28:1 at 48 m.p.h. Stalling speed - 30 m.p.h. Sinking velocity - 6.5 ft./sec. at 70 m.p.h. Wing Area -125 sq. ft. Weight empty - 280 lbs Gross weight - 470 lbs. Aspect ratio - I: 17 Intermediate ribs installed to support the top surface profile 12” 10” 10” 10” 2” 4” 9’8” 9’8” 10” 10” 10” 12” 10” 10” 4’ Chord 2’ 46’ 20’6” 2’ 3’ Late Fuselage with full skid, blown canopy and high tailplane Early Fuselage with simple skid, landing wheel, panelled canopy and low tailplane Drawn by: Vincent Cockett - 2016 © 0 6” 1 2 3 4ft Ross - Stephens RS-1 NACA2418 NACA2412 NACA2416 Late Wing Early Wing Aileron split in half with Inboard section fixed to the wing Early Tailplane Late Tailplane 4’ 7 Dihedral Note: There are other slight variations on the canopies shown

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Skid contains 12 tennis Ballsas part of the suspension

1936

Minimum sinking velocity - 2.5 ft./sec. at 38 m.p.h. Maximum gliding angle - Approx. 28:1 at 48 m.p.h. Stalling speed - 30 m.p.h.Sinking velocity - 6.5 ft./sec. at 70 m.p.h.Wing Area -125 sq. ft. Weight empty - 280 lbs Gross weight - 470 lbs. Aspect ratio - I: 17

Intermediate ribs installed to support the top surface profile

12”

10”

10”

10”

2”

4”

9’8”

9’8”

10”

10”

10”

12”

10”

10”

4’ Chord

2’

46’

20’6”

2’

3’

Late Fuselage withfull skid, blown canopy and high tailplane

Early Fuselage withsimple skid, landing wheel, panelled canopy and low tailplane

Drawn by: Vincent Cockett - 2016 ©

0 6” 1 2 3 4ft Ross - Stephens RS-1

NACA2418

NACA2412

NACA2416

Late Wing

Early Wing

Aileron split in half with Inboard section fixed to the wing

Early Tailplane

Late Tailplane

4’

7 Dihedral

Note: There are other slight variations on the canopies shown