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Titlebook: Re-entry and Planetary Entry Physics and Technology; I / Dynamics, Physic W. H. T. Loh,W. H. T. Loh Book 1968 Springer-Verlag New York Inc.

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书目名称Re-entry and Planetary Entry Physics and Technology
副标题I / Dynamics, Physic
编辑W. H. T. Loh,W. H. T. Loh
视频video
丛书名称Applied Physics and Engineering
图书封面Titlebook: Re-entry and Planetary Entry Physics and Technology; I / Dynamics, Physic W. H. T. Loh,W. H. T. Loh Book 1968 Springer-Verlag New York Inc.
描述During the last decade, a rapid growth of knowledge in the field of re-entry and planetary entry has resulted in many significant advances useful to the student, engineer and scientist. The purpose of offering this course is to make available to them these recent significant advances in physics and technology. Accordingly, this course is organized into five parts: Part 1, Entry Dynamics, Thermodynamics, Physics and Radiation; Part 2, Entry Abla­ tion and Heat Transfer; Part 3, Entry Experimentation; Part 4, Entry Concepts and Technology; and Part 5, Advanced Entry Programs. It is written in such a way so that it may easily be adopted by other universities as a textbook for a two semesters senior or graduate course on the sub­ ject. In addition to the undersigned who served as the course instructor and wrote Chapters, 1, 2, 3 and 4, guest lecturers included: Prof. FRANKLIN K. MOORE who wrote Chapter 5 "Entry Radiative Transfer," Prof. SHIH-I PAl who wrote Chapter 6 "Entry Radiation-Magnetogasdy­ namics," Dr. CARL GAZLEY, Jr. who wrote Chapter 7 "Entry Deaccelera­ tion and Mass Change of an Ablating Body," Dr. SINCLAIRE M. SCALA who wrote Chapter 8 "Entry Heat Transfer and Material R
出版日期Book 1968
关键词dynamics; heat; material; physics; radiation; technology; thermodynamics
版次1
doihttps://doi.org/10.1007/978-3-642-48927-3
isbn_softcover978-3-642-48929-7
isbn_ebook978-3-642-48927-3Series ISSN 0066-5509
issn_series 0066-5509
copyrightSpringer-Verlag New York Inc. 1968
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978-3-642-48929-7Springer-Verlag New York Inc. 1968
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Re-entry and Planetary Entry Physics and Technology978-3-642-48927-3Series ISSN 0066-5509
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Entry Radiative Transferdominant part of the heat load to be withstood by the ablative surface. Kivel. compared convective and radiative heat loads for an ICBM entering at about 20,000 ft/sec and for a Mars probe entering at about 40,000 ft/sec. Figures 5-1 and 5-2 are sketched from Kivel’s paper:
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Entry Mechanics and DynamicsThe equations of motion of a vehicle entering a planet’s atmosphere have been derived by many authors. We shall use them in the form given by Lees, et al. (Ref. 8).
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Carl Gazley Jr.ced to the country through the trading operations of the British East India Company and spread through religious and educational activities from the early nineteenth century on. Until the country achieved her independence from British rule in 1957, the greatest social and economic advantages came wi
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Summary Discussion on Re-entry and Planetary Entry—Physics and Technologyeration, aerodynamic heating and control of the time and location of landing. For non-atmospheric planets, the problem essentially involves only deceleration and control of the time and location of landing. A general description of atmospheric and non-atmospheric planetary entry precedes the analyses of the problem.
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