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A flight determination of the tolerable range of effective dihedral on a conventional fighter airplane

Author: Charles J Liddell; Rudolph D Van Dyke; Donovan R Heinle; United States. National Advisory Committee for Aeronautics.
Publisher: Washington, D.C. : National Advisory Committee for Aeronautics, 1949.
Series: Technical note (United States. National Advisory Committee for Aeronautics), no. 1936.
Edition/Format:   Print book : National government publication : EnglishView all editions and formats
Summary:
A conventional fighter airplane was equipped with a special device for varying the effective dihedral in flight. A survey of pilot's opinions was made to determine which values of effective dihedral were intolerable. The relation between the findings and the present Air Force-Navy stability and control specifications is discussed.
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Additional Physical Format: Online version:
Liddell, Charles J.
Flight determination of the tolerable range of effective dihedral on a conventional fighter airplane.
Washington, D.C. : National Advisory Committee for Aeronautics, 1949
(OCoLC)885175138
Material Type: Government publication, National government publication
Document Type: Book
All Authors / Contributors: Charles J Liddell; Rudolph D Van Dyke; Donovan R Heinle; United States. National Advisory Committee for Aeronautics.
OCLC Number: 660737559
Notes: "August 1949."
NACA TN No. 1936.
Description: 25 pages : illustrations ; 28 cm.
Series Title: Technical note (United States. National Advisory Committee for Aeronautics), no. 1936.
Other Titles: Technical Report Archive & Image Library (TRAIL)
Responsibility: Charles J. Liddell, Jr., Rudolph D. Van Dyke, Jr., and Donovan R. Heinle.

Abstract:

A conventional fighter airplane was equipped with a special device for varying the effective dihedral in flight. A survey of pilot's opinions was made to determine which values of effective dihedral were intolerable. The relation between the findings and the present Air Force-Navy stability and control specifications is discussed.

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