Complete tank tests of two flying-boat hulls with pointed steps - N.A.C.A. Models 22-A and 35 / by James M. Shoemaker and Joe W. Bell.

Format:

Book

Government document

Author/Creator:

Shoemaker, J. M. (James Maurice), author.

Bell, Joe W., author.

Contributor:

United States. National Advisory Committee for Aeronautics, issuing body.

Series:

Technical note (United States. National Advisory Committee for Aeronautics) ; 504.

Technical note / National Advisory Committee for Aeronautics ; No. 504

Language:

English

Subjects (All):

Seaplanes--Hulls.

Seaplanes.

Seaplanes--Testing.

Physical Description:

1 online resource (21 pages, 15 unnumbered pages) : illustrations.

Place of Publication:

Washington, [D.C.] : National Advisory Committee for Aeronautics, 1934.

Summary:

This note presents the results of complete tank tests of N.A.C.A. models 22-A and 35, two flying-boat hulls of the deep pointed-step type with low dead rise.

Take-off examples are worked out using data from these tests and a previous test of a conventional model applied to an arbitrary set of design specifications for a 15,000-pound flying boat. The comparison of these examples shows both pointed-step models to be superior to the conventional form, and Model 35 to be the better of the two.

Notes:

Title from title screen (viewed March 18, 2020).

"September 1934."

"Langley Memorial Aeronautical Laboratory."

No Federal Depository Library Program (FDLP) item number.

Includes bibliographical references (pages 13-14).

Electronic reproduction. Denton, Texas : University of North Texas, 2011. Electronic reproduction from print master produced by University of North Texas.

Other Format:

Print version: Shoemaker, J. M. (James Maurice). Complete tank tests of two flying-boat hulls with pointed steps - N.A.C.A. Models 22-A and 35.

OCLC:

1145759603