Academic Journal

Predicting the Initial Crack Length in a Solid Propellant

التفاصيل البيبلوغرافية
العنوان: Predicting the Initial Crack Length in a Solid Propellant
المؤلفون: Liu, C. T., Kwon, Y. G., Hendrickson, T. L.
المساهمون: AIR FORCE RESEARCH LAB EDWARDS AFB CA SPACE AND MISSILE PROPULSION DIV
المصدر: DTIC AND NTIS
سنة النشر: 2001
المجموعة: Defense Technical Information Center: DTIC Technical Reports database
مصطلحات موضوعية: Solid Rocket Propellants, STRESS STRAIN RELATIONS, SOLID PROPELLANTS, CRACKS, MATHEMATICAL PREDICTION, CRACK LENGTHS, PRESENTATION SLIDES, VIEWGRAPHS ONLY, WUAFRL2303M1G2346120
الوصف: Prepared in collaboration with Naval Postgraduate School and Thiokol Co. Presented at the JANNAF Structures and Mechanical Behavior Subcommittee Meeting (34th) held in Cocoa Beach, FL on 26-30 March 2001.
نوع الوثيقة: text
وصف الملف: text/html
اللغة: English
Relation: http://www.dtic.mil/docs/citations/ADA410508
الاتاحة: http://www.dtic.mil/docs/citations/ADA410508
http://oai.dtic.mil/oai/oai?&verb=getRecord&metadataPrefix=html&identifier=ADA410508
Rights: APPROVED FOR PUBLIC RELEASE
رقم الانضمام: edsbas.464C922C
قاعدة البيانات: BASE