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PROJECT FIRE FLIGHT 1 HEATING AND PRESSURE MEASUREMENTS ON THE REENTRY-VEHICLE AFTERBODY AT A VELOCITY OF 38,000 FEET PER SECOND

机译：项目消防飞行1在每秒38,000英尺的速度下对再造车辆后的加热和压力测量

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作者
SLOCUMB, T. H., JR.;
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年度 1965
页码 1-47
总页数 47
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AERODYNAMIC HEATING; AFTERBODIES; PRESSURE MEASUREMENT; REENTRY VEHICLES; BLUNT BODIES;

机译：空气动力加热; aFTERBODIEs;压力测量; REENTRY车辆; BLUNT BODIEs;

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1. Aerodynamic Heating Measurement on Afterbody of Hypersonic Flight Experiment [J] . Keisuke Fujii, Yasutoshi Inoue Journal of Spacecraft and Rockets . 1998,第6期

机译：高超音速飞行器尾气气动加热测量
2. Afterbody Aeroheating Flight Data for Planetary Probe Thermal Protection System Design [J] . Michael J. Wright, Frank S. Milos, Philippe Tran Journal of Spacecraft and Rockets . 2006,第5期

机译：用于行星式探头热保护系统设计的车身后热飞行数据
3. Pressure, temperature and free-flight projectile-displacement measurements during a plasma discharge generated on a supersonic projectile [J] . Patrick Gnemmi, Christian Rey, Alfred Eichhorn, International Journal of Aerodynamics . 2013,第1a3期

机译：在超音速弹丸上产生等离子体放电期间的压力，温度和自由飞行弹丸位移测量
4. Viking Afterbody Heating Computations and Comparisons to Flight Data [C] . K. Edquist, M. Wright, G. Allen AIAA Aerospace Sciences Meeting and Exhibit . 2006

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5. A Methodology for the Development of Direct Fired Flight Projectiles [D] . Farina, Anthony P. 2010

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6. High-Pressure Geoscience Special Feature: Indoor seismology by probing the Earths interior by using sound velocity measurements at high pressures and temperatures [O] . Baosheng Li, Robert C. Liebermann 2007

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8. Forebody temperatures and total heating rates measured during Project Fire 1 reentry at 38,000 feet per second [R] . Cornette, E. S. 1965

机译：在project Fire 1期间测量的前体温度和总加热速率为38,000英尺/秒

PROJECT FIRE FLIGHT 1 HEATING AND PRESSURE MEASUREMENTS ON THE REENTRY-VEHICLE AFTERBODY AT A VELOCITY OF 38,000 FEET PER SECOND

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