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Contents

   



(Top)
 


1 Design and development  





2 Operational history  





3 Specifications (GW-7)  





4 See also  





5 References  














Whigham GW-7







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From Wikipedia, the free encyclopedia
 


GW-7
Role Glider
National origin United States
Designer Gene Whigham
First flight 1987
Status No longer in production
Number built one

The Whigham GW-7 is an American mid-wing, single-seat, 15 metre class glider that was designed and constructed by Gene Whigham, a retired Convair flight test engineer.[1][2]

Design and development

[edit]

Whigham's last glider design was the GW-7. The aircraft was completed and first flew in 1987.[1][2]

The GW-7 is of all metal construction, has a 15 m (49.2 ft) wing span and employs a NASA NLF(1)-0215F airfoil. The flaps and ailerons are interconnected. The flaps travel +/-10° in normal flight in concert with the ailerons and then can be deployed to 60° for glidepath control on landing.[1][3]

Only one GW-7 was constructed and it was registered with the Federal Aviation Administration as an Experimental - Amateur-built.[2]

Operational history

[edit]

In July 2011 the sole GW-7 built was still on the FAA registry and owned by Donald Macey of Fallon, Nevada.[2]

Specifications (GW-7)

[edit]

Data from Sailplane Directory[1]

General characteristics

Performance

See also

[edit]

Related lists

References

[edit]
  1. ^ a b c d Activate Media (2006). "GW-7 Whigham". Retrieved July 5, 2011.
  • ^ a b c d Federal Aviation Administration (July 2011). "Make / Model Inquiry Results N6198". Retrieved July 5, 2011.
  • ^ Lednicer, David (2010). "The Incomplete Guide to Airfoil Usage". Archived from the original on April 20, 2010. Retrieved July 1, 2011.

  • Retrieved from "https://en.wikipedia.org/w/index.php?title=Whigham_GW-7&oldid=1144172570"

    Categories: 
    1980s United States sailplanes
    Homebuilt aircraft
    Aircraft first flown in 1987
    Mid-wing aircraft
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    This page was last edited on 12 March 2023, at 06:01 (UTC).

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