GW-2, GW-4 and GW-5 Whigham   


Click on an image to see a full size photograph
General Details
Manufacturer: Whigham
Plane Name:

GW-2, GW-4 and GW-5

Classified as: Unclassified
Country Of Origin: U S A
Designer: Eugene Whigham
No. of Seats 1
No. Built 0
   
Performance:
L/DMax: 33
   
MinSink:
   


 

Specifications:
Span Area Empty Weight Payload Gross Weight Wing Load Water Ballast
m ft sq.m sq.ft kg lb. kg lb. kg lb. kg
/sq.m
lb.
/sq.ft
kg lb.
15 49.2 12.17 131 235 518 115 252 350 770 28.76 5.87 0 0
Aspect ratio: 18.5
Airfoil: Wortmann 61-184
Structure: all metal, fabric cover on wing aft of spar
Engine:

Comment:
The GW-2, which first flew in 1964, was the result of experience gained with the GW-1, and featured a longer (16.15 m./ 53.0 ft.) NACA 63(3) 618 section high aspect ratio wing with spoilers, V-tail, fixed wheel and skid. The GW-3 was developed from the ヨ2 with an emphasis on simplicity. It had a NACA 4301 2A airfoil and flaps. The GW-4 followed on from the ヨ3 with a higher wing loading of 30.66 kg./ sq. m/ 6.28 lb./ sq. ft. The GW-5 used a constant chord 15 m. wing to qualify as a Standard Class ship. As with the earlier models the ヨ5 has a faired fixed landing gear. Flaps, are provided for glidepath control, and the tail is conventional. Specifications are for the GW-5


           

Your Comments:

Sailplanedirectory.com Copyright 2006 Activate Media. Glider data contains information Copyright www.ssa.org.