المؤلفون: Qu Youwen, An Xiaomin, Deng Bin, Yan Hao, Zhou Yue

المصدر: Hangkong bingqi, Vol 29, Iss 4, Pp 91-99 (2022)

مصطلحات موضوعية: hypersonic velocity, panel flutter, composite materials, thermal effect, nonlinear aeroelasticity, thermal buckling, vehicle, Motor vehicles. Aeronautics. Astronautics, TL1-4050

وصف الملف: electronic resource

العلاقة: https://www.aeroweaponry.avic.com/fileup/1673-5048/PDF/2021-00183.pdfTest; https://doaj.org/toc/1673-5048Test

الوصول الحر: https://doaj.org/article/9f7f7282e7fb46a9b480f981e15484c3Test

المؤلفون: V. L. Balakin, M. M. Krikunov

المصدر: Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 18, Iss 1, Pp 18-29 (2019)

مصطلحات موضوعية: Aerospace system, first stage, climb, acceleration, hypersonic velocity, angle-of-attack, propellant mass minimum, maximum principle method, dynamic pressure, heat flux, Motor vehicles. Aeronautics. Astronautics, TL1-4050

وصف الملف: electronic resource

العلاقة: https://journals.ssau.ru/index.php/vestnik/article/view/6530Test; https://doaj.org/toc/2542-0453Test; https://doaj.org/toc/2541-7533Test

الوصول الحر: https://doaj.org/article/3cd241284b55465c9a6494ef12119d85Test

المؤلفون: Balakin V.L., Krikunov M.M.

المصدر: VESTNIK of Samara University. Aerospace and Mechanical Engineering; Vol 18, No 1 (2019); 18-29 ; Вестник Самарского университета. Аэрокосмическая техника, технологии и машиностроение; Vol 18, No 1 (2019); 18-29 ; 2541-7533 ; 2542-0453

مصطلحات موضوعية: Авиационно-космическая система, первая ступень, набор высоты, разгон, гиперзвуковая скорость, угол атаки, минимум массы топлива, метод принципа максимума, скоростной напор, тепловой поток, Aerospace system, first stage, climb, acceleration, hypersonic velocity, angle-of-attack, propellant mass minimum, maximum principle method, dynamic pressure, heat flux

وصف الملف: application/pdf

العلاقة: https://journals.ssau.ru/vestnik/article/view/6530/7263Test; https://journals.ssau.ru/vestnik/article/view/6530Test

الإتاحة: https://doi.org/10.18287/2541-7533-2019-18-1-18-29Test
https://journals.ssau.ru/vestnik/article/view/6530Test

المؤلفون: Xiang-yu Zhang, Guo-hong Wang, Zhen-yu Song, Jiao-jiao Gu

المصدر: Defence Technology, Vol 11, Iss 4, Pp 370-381 (2015)

مصطلحات موضوعية: Near space, Hypersonic velocity, High dynamic bias, Tracking, Maneuvering, Military Science

وصف الملف: electronic resource

العلاقة: http://www.sciencedirect.com/science/article/pii/S2214914715000380Test; https://doaj.org/toc/2214-9147Test

الوصول الحر: https://doaj.org/article/507ca6c718cb4472bbda5a48d384a95bTest

المؤلفون: Zhen-yu Song, Jiao-jiao Gu, Xiang-yu Zhang, Guo-hong Wang

المصدر: Defence Technology, Vol 11, Iss 4, Pp 370-381 (2015)

مصطلحات موضوعية: Hypersonic speed, ECEF, Computer science, Hypersonic velocity, Mechanical Engineering, Tracking, Metals and Alloys, Computational Mechanics, Filter (signal processing), Maneuvering, Tracking (particle physics), Near space, Radial velocity, Acceleration, Military Science, Control theory, Ceramics and Composites, High dynamic bias, Divergence (statistics)

الوصول الحر: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::2787a88314774ff70396660117a42d32Test
http://www.sciencedirect.com/science/article/pii/S2214914715000380Test

المؤلفون: Hongmin Zhu, Mamoru Endo, Tsutomu Yamamura, Yoshiyuki Sato, Yuzuru Sato

المصدر: ISIJ International. 1993, 33(1):176

المؤلفون: Tatsuhiko Ejima, 江島 辰彦

المصدر: 日本金属学会会報 / Bulletin of the Japan Institute of Metals. 1983, 22(11):962

المؤلفون: Sheaffer, Patti M, Adams, Paul M, Hemmi, Naoki, Hartney, Christopher

المساهمون: AEROSPACE CORP EL SEGUNDO CA

المصدر: DTIC

مصطلحات موضوعية: Explosions, Fluid Mechanics, Unmanned Spacecraft, FRAGMENTATION, HYPERSONIC VELOCITY, LAUNCH VEHICLES, HYPERVELOCITY IMPACT, LABORATORIES, MECHANICS, PHYSICAL PROPERTIES, TARGETS, TEST AND EVALUATION, DEBRISLV, droit, geo

العلاقة: http://www.dtic.mil/docs/citations/ADA625015Test

الإتاحة: http://www.dtic.mil/docs/citations/ADA625015Test

المؤلفون: Leyva, Ivett

المساهمون: AIR FORCE RESEARCH LAB EDWARDS AFB CA AEROSPACE SYSTEMS DIRECTORATE

المصدر: DTIC

مصطلحات موضوعية: Inorganic Chemistry, Acoustics, ACOUSTICS, BOUNDARY LAYER, CARBON DIOXIDE, HYPERSONIC VELOCITY, CHEMICALS, CONFIGURATIONS, ENERGY, ENERGY ABSORBERS, FLOW, FREQUENCY, GROWTH(GENERAL), INJECTION, INSTABILITY, INTERACTIONS, MOLECULES, MOTIVATION, NONEQUILIBRIUM FLOW, PURITY, RELAXATION, TRANSITIONS, VIBRATION, Q0AF

وصف الملف: text/html

العلاقة: http://www.dtic.mil/docs/citations/ADA598071Test

الإتاحة: http://www.dtic.mil/docs/citations/ADA598071Test
http://oai.dtic.mil/oai/oai?&verb=getRecord&metadataPrefix=html&identifier=ADA598071Test

المؤلفون: Savelkin,, K V, Yarantsev, D A, Adamovich, I V, Leonov, S B

المساهمون: OHIO STATE UNIV COLUMBUS DEPT OF MECHANICAL AND AEROSPACE ENGINEERING

المصدر: DTIC

مصطلحات موضوعية: Electricity and Magnetism, Plasma Physics and Magnetohydrodynamics, Combustion and Ignition, Jet and Gas Turbine Engines, ELECTRIC DISCHARGES, FUEL INJECTORS, SUPERSONIC COMBUSTION RAMJET ENGINES, AERODYNAMICS, BOUNDARY LAYER FLOW, COMPRESSION IGNITION, ETHYLENE, FLOW FIELDS, HYPERSONIC VELOCITY, JET FLAMES, MACH NUMBER, NONEQUILIBRIUM FLOW, PLASMAS(PHYSICS), REACTION KINETICS, STAGNATION PRESSURE, IGNITION TIME, SCRAMJET COMBUSTORS

وصف الملف: text/html

العلاقة: http://www.dtic.mil/docs/citations/ADA615888Test

الإتاحة: http://www.dtic.mil/docs/citations/ADA615888Test
http://oai.dtic.mil/oai/oai?&verb=getRecord&metadataPrefix=html&identifier=ADA615888Test