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W. H. T. Loh

Re-entry and Planetary Entry Physics and Technology


I / Dynamics, Physics, Radiation, Heat Transfer and Ablation
Herausgegeben von Loh, W.H.T.
Softcover reprint of the original 1st ed. 1968. 2012. viii, 488 S. VIII, 487 pp. 252 figs. 229 mm
Verlag/Jahr: SPRINGER, BERLIN 2012
ISBN: 3-642-48929-X (364248929X)
Neue ISBN: 978-3-642-48929-7 (9783642489297)

Preis und Lieferzeit: Bitte klicken


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 Response," Mr.
1. Summary Discussion on Re-entry and Planetary Entry: Physics and Technology.- One. Entry Dynamics, Thermodynamics, Physics and Radiation.- 2. Entry Mechanics.- 3. Entry Thermodynamics.- 4. Orbital and Celestial Mechanics.- 5. Entry Radiative Transfer.- 6. Entry Radiation-Magnetogasdynamics.- Two. Entry Ablation and Heat Transfer.- 7. Entry Deceleration and Mass Change of an Ablating Body.- 8. Entry Heat Transfer and Material Response.