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 -- 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