Real-time testing of titanium sheet and extrusion coupon specimens subjected to Mach 2.7 supersonic cruise aircraft wing stresses and temperatures
By: Tjerand Lunde, Lockheed-California Company ; prepared for Langley Research Center.
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.; Lockheed-California Company.
Series: NASA contractor report ; 2754; NASA contractor report -- NASA CR-2754.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office
Published: 1977
Place of publication: [Washington]
Language: eng
Number of pages: 94
Subjects: Materials -- Fatigue.; Titanium alloys -- Fatigue.
Notes: Contract NAS 1-13649.

Dec. 1977.

Includes bibliographical references.