دورية أكاديمية

Notes on Analytical Techniques in Aerodynamic Heating Problems

التفاصيل البيبلوغرافية
العنوان: Notes on Analytical Techniques in Aerodynamic Heating Problems
المؤلفون: JOHNSON, C H, SMITH, WILLIAM H, KATZ, J R
المساهمون: NAVAL ORDNANCE TEST STATION CHINA LAKE CA
المصدر: DTIC AND NTIS
سنة النشر: 1961
المجموعة: Defense Technical Information Center: DTIC Technical Reports database
مصطلحات موضوعية: Fluid Mechanics, AERODYNAMIC HEATING, ANALOG COMPUTERS, GUIDED MISSILES, HEAT TRANSFER, FUNCTIONS(MATHEMATICS), HEATING, MATHEMATICAL ANALYSIS, MODEL TESTS, NOSE CONES, PARTIAL DIFFERENTIAL EQUATIONS, PROPELLANT GRAINS, ROCKET ENGINES, ROCKET PROPELLANTS, SIMULATION, SURFACE TEMPERATURE, TEMPERATURE, TEST METHODS, THERMAL INSULATION, THICKNESS, sidewinder, hpag rocket motor
الوصف: TEMPERATURE CHANGES DURING HEATING OF AN HPAG 5.0-INCH MOTOR: CORRELATION OF EXPERIMENTAL DATA WITH ANALOG COMPUTATIONS, by C. H. Johnson: Temperature data on a 5.0-inch HPAG rocket motor served to guide the set up of an analog computer model. The study was prompted by observations that temperatures in heated Sidewinder 1C motors differed appreciably depending on whether the test point was at the top, side, or bottom of the motor. DETERMINATION OF WALL TEMPERATURE-TIME FUNCTIONS USING AN ANALOG COMPUTER, by William H. Smith: The use of an analog computer to obtain solutions of the outside surface temperature of aerodynamically heated bodies resulted in a large saving over hand solutions. WHEN IS A SKIN THERMALLY THIN, by Jerome R. Katz: A method for determining skin thickness is discussed for 1, 5, and 10% variations in temperature throughout the material.
نوع الوثيقة: text
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اللغة: English
العلاقة: http://www.dtic.mil/docs/citations/AD0258223Test
الإتاحة: http://www.dtic.mil/docs/citations/AD0258223Test
http://oai.dtic.mil/oai/oai?&verb=getRecord&metadataPrefix=html&identifier=AD0258223Test
حقوق: Approved for public release; distribution is unlimited.
رقم الانضمام: edsbas.4A95890E
قاعدة البيانات: BASE