Titanium honeycomb panel testing / W. Lance Richards, Randolph C. Thompson.

Format:

Book

Government document

Author/Creator:

Richards, W. Lance, author.

Thompson, Randolph C., author.

Contributor:

Hugh L. Dryden Flight Research Center

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program, issuing body.

United States. National Aeronautics and Space Administration, sponsoring body.

Series:

NASA technical memorandum ; 4768.

NASA technical memorandum ; 4768

Language:

English

Subjects (All):

Honeycomb structures.

Genre:

NASA Technical Memorandum

Physical Description:

1 online resource (17 pages) : illustrations.

Place of Publication:

[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, October 1996.

Summary:

Thermal-mechanical tests were performed on a titanium honeycomb sandwich panel to experimentally validate the hypersonic wing panel concept and compare test data with analysis. Details of the test article, test fixture development, instrumentation, and test results are presented. After extensive testing to 900 deg F, nondestructive evaluation of the panel has not detected any significant structural degradation caused by the applied thermal-mechanical loads.

Notes:

Title from title screen (viewed March 2, 2016).

"October 1996."

"Performing organization: NASA Dryden Flight Research Center , Edwards, California"--Report documentation page.

Includes bibliographical references (page 5).

pdf http://dtrs.dfrc.nasa.gov/archive/00000203/01/TM4768.pdf

Other Format:

Microfiche version: Richards, W. Lance. Titanium honeycomb panel testing

OCLC:

703660806