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Book Ignition of Mixtures of SiH4  CH4  O2  and Ar Or N2 Behind Reflected Shock Waves

Download or read book Ignition of Mixtures of SiH4 CH4 O2 and Ar Or N2 Behind Reflected Shock Waves written by Allen G. McLain and published by . This book was released on 1985 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Ignition of SiH4 H2 O2 N2 Behind Reflected Shock Waves

Download or read book Ignition of SiH4 H2 O2 N2 Behind Reflected Shock Waves written by Allen G. McLain and published by . This book was released on 1983 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Ignition of SiH4 H2 02 N2 Behind Reflected Shock Waves

Download or read book Ignition of SiH4 H2 02 N2 Behind Reflected Shock Waves written by Allen G. McLain and published by . This book was released on 1983 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book NASA Technical Paper

Download or read book NASA Technical Paper written by and published by . This book was released on 1985 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Ignition Delay Times and Structure of Detonation Waves in CH4 O2 N2 and H2 O2 N2 Mixtures

Download or read book Ignition Delay Times and Structure of Detonation Waves in CH4 O2 N2 and H2 O2 N2 Mixtures written by and published by . This book was released on 1999 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: Simplified chemical-kinetic mechanisms and reduced chemical-kinetic mechanisms were developed for describing structure of the dark zone formed over the burning surface of double base and nitramine propellants. It is believed that ignition delays in large caliber gun ballistic cycles are related to the chemistry taking place in the dark zone. Ignition delay times calculated using the simplified mechanisms were found to agree well with those calculated using detailed chemical-kinetic mechanisms. The simplified mechanisms are expected to be useful in interior ballistics calculations. Reduced chemical-kinetic mechanisms were developed to calculate the structures of premixed and nonpremixed flames burning various hydrocarbon fields. Asymptotic analyses were performed using the reduced mechanisms. Burning velocities of premixed flames and critical conditions of extinction of nonpremixed flames were calculated using results of the asymptotic analyses. Simplified chemical-kinetic mechanisms were developed for calculating ignition delay times in combustible mixtures used in the Ram Accelerator. The results of all these studies are described in eight journal articles and five technical reports published in proceedings of technical meetings.

Book AIAA 86 1374   AIAA 86 1438  v  2   AIAA 86 1440   AIAA 86 1499

Download or read book AIAA 86 1374 AIAA 86 1438 v 2 AIAA 86 1440 AIAA 86 1499 written by and published by . This book was released on 1986 with total page 636 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book AIAA Aerospace Sciences Meeting and Exhibit  42nd

Download or read book AIAA Aerospace Sciences Meeting and Exhibit 42nd written by and published by . This book was released on 2004 with total page 580 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book The Aeronautical Journal

Download or read book The Aeronautical Journal written by and published by . This book was released on 1985 with total page 504 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Shock induced Ignition of High pressure H2 O2 Ar and CH4 O2 Ar Mixtures

Download or read book Shock induced Ignition of High pressure H2 O2 Ar and CH4 O2 Ar Mixtures written by E. L. Peterson and published by . This book was released on 1995 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Shock Initiated Ignition in Heptane Oxygen Argon Mixtures

Download or read book Shock Initiated Ignition in Heptane Oxygen Argon Mixtures written by Alexander Burcat and published by . This book was released on 1981 with total page 8 pages. Available in PDF, EPUB and Kindle. Book excerpt: The ignition of heptane in mixtures containing oxygen and argon was studied behind reflected shock waves in 56 mm i.d. and 26 mm i.d. single-pulse shock tubes. The measurements covered the temperature range 1100-1700 K and reflected shock pressures varying from 2 to 12 atmospheres.

Book Mass Independent Isotopic Fractionation in Solid Phase

Download or read book Mass Independent Isotopic Fractionation in Solid Phase written by Xianping Xu and published by . This book was released on 1998 with total page 334 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book International Aerospace Abstracts

Download or read book International Aerospace Abstracts written by and published by . This book was released on 1993 with total page 1146 pages. Available in PDF, EPUB and Kindle. Book excerpt: