Effect of Increase in Angle of Dead Rise on the Hydrodynamic Qualities of a Seaplane Configuration Incorporating High Wing Loading Page: 1 of 33
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EFFECT OF INCREASE IN ANGLE OF DEAD RISE ON THE
HYDRODYNAMIC QUALITIES OF A SEAPLANE CONFIGURATION
INCORPORATING IG-H WING LOADING
By Walter J. Kapryan and Irving Weinstein
Langley Aeronautical Laboratory
CLASSIFICATION WWt4 Jd, Va. LR YCd, Vp.
To... _-4--AgSgF4-D...-.---. ----. NOV 2 1956
De re.. LANGLEY AE NAIC A
By authorLty ...ANALEY FIELD, VIRGINIA
CL ASSISED DOCUMENT-
This material contains information atecting the Natona Deense of the United States within the r.eansg
of the espicmage laws, Title S8, U.S.C., Secs. 793 ad 7924, the tranmssion or revelatoa of which in any
manner to an unauthori zed person is prohibited by lar.
NATIONAL ADVISORY COMMITTEE
October 31, 1956
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Kapryan, Walter J. & Weinstein, Irving. Effect of Increase in Angle of Dead Rise on the Hydrodynamic Qualities of a Seaplane Configuration Incorporating High Wing Loading, report, October 31, 1956; (digital.library.unt.edu/ark:/67531/metadc62936/m1/1/: accessed November 20, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.