Titlebook: A Theory of Supercritical Wing Sections, with Computer Programs and Examples; With Computer Progra Frances Bauer,Paul Garabedian,David Korn

遮蔽

書目名稱A Theory of Supercritical Wing Sections, with Computer Programs and Examples影響因子(影響力)




書目名稱A Theory of Supercritical Wing Sections, with Computer Programs and Examples影響因子(影響力)學(xué)科排名




書目名稱A Theory of Supercritical Wing Sections, with Computer Programs and Examples網(wǎng)絡(luò)公開度




書目名稱A Theory of Supercritical Wing Sections, with Computer Programs and Examples網(wǎng)絡(luò)公開度學(xué)科排名




書目名稱A Theory of Supercritical Wing Sections, with Computer Programs and Examples被引頻次




書目名稱A Theory of Supercritical Wing Sections, with Computer Programs and Examples被引頻次學(xué)科排名




書目名稱A Theory of Supercritical Wing Sections, with Computer Programs and Examples年度引用




書目名稱A Theory of Supercritical Wing Sections, with Computer Programs and Examples年度引用學(xué)科排名




書目名稱A Theory of Supercritical Wing Sections, with Computer Programs and Examples讀者反饋




書目名稱A Theory of Supercritical Wing Sections, with Computer Programs and Examples讀者反饋學(xué)科排名

難理解

Examples,von Maschinen und Anlagen sind h?ufig Resultate hydraulischer und pneumatischer Antriebs- und Steuerungstechnik. Bei linearen wie auch rotatorischen Bewegungen, gleichm??igen Huboder Senkbewegungen, Beschleunigungsforderungen, Leistungsübertragungen oder dem Bedarf Positionen anzufahren und zu halte

Ancillary

起波瀾

hurricane

Examples,Maschine oder ein Flugzeug bewegt sich ohne sie – nur ist es uns meistens nicht bewusst. Die Hydraulikund Pneumatikhersteller sind Zulieferer für die gesamte Industrie. Zu ihren Abnehmerbranchen z?hlen z. B. die Automobilindustrie, die Baumaschinen- und Landmaschinenindustrie, die F?rdertechnik, die

Asperity

SYN

Book 1972 we include a turbulent boundary layer correction. Part I of the paper is devoted to a description of the mathemati- cal theory and need not be studied by those primarily concerned with running the programs. Part II is a manual for users of our programs which is independent of the theoretical part.

Addictive

大量

Dying as liminality in the making,ying this manual it should be possible to learn how to operate the design and analysis programs even with only a limited understanding of the mathematical content. We intend to make the basic method available to those interested in designing transonic airfoils but unwilling to spend the time require

無表情

https://doi.org/10.1057/978-1-137-53849-9numbers of test runs of the program to produce, with the earliest case requiring hundreds of trials, but the later ones needing less as we gained experience. All models were designed to have a maximum thickness-chord ratio T/C for given free stream Mach number M. and lift coefficient C., subject to