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商品	説明	価格
Transonic Communicator【電子書籍】[ Glen C. Cutlip ] 楽天Kobo電子書籍ストア	＜p＞Within the Transonic Communicator, one finds a means of Communication that transcends communication itself without doing so. Transonic Communication is a communication that takes place within one’s threefold Christ Self with the Consciousness of God. It’s an interactive communication, not a one way thing. One must participate in the communication.＜/p＞画面が切り替わりますので、しばらくお待ち下さい。 ※ご購入は、楽天kobo商品ページからお願いします。※切り替わらない場合は、こちらをクリックして下さい。 ※このページからは注文できません。	452円
【中古】Mathematical Aspects of Subsonic and Transonic Gas Dynamics (Dover Books on Physics) ブックサプライ	◇◆主にゆうメールによるポスト投函、サイズにより宅配便になります。◆梱包：完全密封のビニール包装または宅配専用パックにてお届けいたします。◆帯、封入物、及び各種コード等の特典は無い場合もございます◆◇【10164】全商品、送料無料！	2,200円
Unsteady Transonic Flow【電子書籍】[ Marten T. Landahl ] 楽天Kobo電子書籍ストア	＜p＞This classic monograph on unsteady transonic flow ー the flow of air encountered at speeds at or near the speed of sound ー is of continuing interest to students and professionals in aerodynamics, fluid dynamics, and other areas of applied mathematics.＜br /＞ After a brief Introduction, Swedish physicist M?rten T. Landahl presents a chapter in which the two-dimensional solution is derived, succeeded by a discussion of its relation to the subsonic and supersonic solutions. Three chapters on low aspect ratio configurations follow, covering triangular wings and similar planforms with curved leading edges, rectangular wings, and cropped delta wings, and low aspect ratio wing-body combinations. The treatment concludes with a consideration of the experimental determination of air forces on oscillating wings at transonic speeds.＜/p＞画面が切り替わりますので、しばらくお待ち下さい。 ※ご購入は、楽天kobo商品ページからお願いします。※切り替わらない場合は、こちらをクリックして下さい。 ※このページからは注文できません。	1,729円
Active Aeroelastic Wing Improve Aircraft Maneuverability at Transonic and Supersonic Speeds【電子書籍】[ Fouad Sabry ] 楽天Kobo電子書籍ストア	＜p＞＜strong＞What Is Active Aeroelastic Wing＜/strong＞＜/p＞＜p＞The X-53 Active Aeroelastic Wing (AAW) development program is an American research project that has been completed. This project was carried out jointly by the Air Force Research Laboratory (AFRL), Boeing Phantom Works, and NASA's Dryden Flight Research Center. At NASA's Dryden Flight Research Center, the technology was flight tested on a modified McDonnell Douglas F/A-18 Hornet. Active Aeroelastic Wing Technology is a technology that blends the aerodynamics, controls, and structure of a wing in order to harness and regulate the aeroelastic twist that a wing experiences under dynamic stresses and high speeds. The use of multiple leading and trailing edge controls, such as "aerodynamic tabs," enables subtle amounts of aeroelastic twist to be controlled to provide large amounts of wing control power, while simultaneously minimizing maneuver air loads under high wing strain conditions or aerodynamic drag under low wing strain conditions. This is accomplished while maintaining a balance between the two extremes of wing strain conditions. This operation served as the very first demonstration of AAW technology on a large scale.＜/p＞＜p＞＜strong＞How You Will Benefit＜/strong＞＜/p＞＜p＞(I) Insights, and validations about the following topics:＜/p＞＜p＞Chapter 1: Active Aeroelastic Wing＜/p＞＜p＞Chapter 2: Aileron＜/p＞＜p＞Chapter 3: Aeroelasticity＜/p＞＜p＞Chapter 4: Elevon＜/p＞＜p＞Chapter 5: NASA X-43＜/p＞＜p＞Chapter 6: List of experimental aircraft＜/p＞＜p＞Chapter 7: Boeing X-45＜/p＞＜p＞Chapter 8: Grumman X-29＜/p＞＜p＞Chapter 9: Air Force Research Laboratory＜/p＞＜p＞Chapter 10: Boeing X-48＜/p＞＜p＞Chapter 11: Elevator (aeronautics)＜/p＞＜p＞Chapter 12: Flap (aeronautics)＜/p＞＜p＞Chapter 13: United States Air Force Stability and Control Digital DATCOM＜/p＞＜p＞Chapter 14: Leading-edge cuff＜/p＞＜p＞Chapter 15: Flaperon＜/p＞＜p＞Chapter 16: Spoileron＜/p＞＜p＞Chapter 17: McDonnell Douglas F-15 STOL/MTD＜/p＞＜p＞Chapter 18: Boeing X-51 Waverider＜/p＞＜p＞Chapter 19: Adaptive compliant wing＜/p＞＜p＞Chapter 20: Leading-edge slat＜/p＞＜p＞Chapter 21: General Dynamics-Boeing AFTI/F-111A Aardvark＜/p＞＜p＞(II) Answering the public top questions about boeing x53 active aeroelastic wing.＜/p＞＜p＞(III) Real world examples for the usage of boeing x53 active aeroelastic wing in many fields.＜/p＞＜p＞(IV) 17 appendices to explain, briefly, 266 emerging technologies in each industry to have 360-degree full understanding of boeing x53 active aeroelastic wing' technologies.＜/p＞＜p＞＜strong＞Who This Book Is For＜/strong＞＜/p＞＜p＞Professionals, undergraduate and graduate students, enthusiasts, hobbyists, and those who want to go beyond basic knowledge or information for any kind of boeing x53 active aeroelastic wing.＜/p＞画面が切り替わりますので、しばらくお待ち下さい。 ※ご購入は、楽天kobo商品ページからお願いします。※切り替わらない場合は、こちらをクリックして下さい。 ※このページからは注文できません。	700円
Introduction to Transonic Aerodynamics【電子書籍】[ Roelof Vos ] 楽天Kobo電子書籍ストア	＜p＞Written to teach students the nature of transonic flow and its mathematical foundation, this book offers a much-needed introduction to transonic aerodynamics. The authors present a quantitative and qualitative assessment of subsonic, supersonic and transonic flow around bodies in two and three dimensions. The book reviews the governing equations and explores their applications and limitations as employed in modeling and computational fluid dynamics.＜/p＞＜p＞Some concepts, such as shock and expansion theory, are examined from a numerical perspective. Others, including shock-boundary-layer interaction, are discussed from a qualitative point of view. The book includes 60 examples and more than 200 practice problems. The authors also offer analytical methods such as Method of Characteristics (MOC) that allow readers to practice with the subject matter.＜/p＞＜p＞The result is a wealth of insight into transonic flow phenomena and their impact on aircraft design, including compressibility effects, shock and expansion waves, shock-boundary-layer interaction and aeroelasticity.＜/p＞画面が切り替わりますので、しばらくお待ち下さい。 ※ご購入は、楽天kobo商品ページからお願いします。※切り替わらない場合は、こちらをクリックして下さい。 ※このページからは注文できません。	10,331円
Toward Mach 2: The Douglas D-558 Program - Skystreak and Skyrocket Early Transonic Research Aircraft (NASA SP-4222)【電子書籍】[ Progressive Management ] 楽天Kobo電子書籍ストア	＜p＞This official NASA history report - converted for accurate flowing-text e-book format reproduction - provides a history of research with the D-558 Skystreak and Skyrocket supersonic airplane at NASA's Dryden Flight Research Center in California.＜/p＞＜p＞In the long and proud history of flight research at what is now called the NASA Dryden Flight Research Center, the D-558 project holds a special place as being one of the earliest and most productive flight research efforts conducted here. Data from the D-558 and the early X-planes enabled researchers at what became NASA's Langley Research Center to correlate and correct test results from wind tunnels with actual flight values. Then, the combined results of flight and wind-tunnel testing enabled the U.S. aeronautical community to solve many of the problems that occur in the transonic speed range (about 0.8 to 1.2 times the speed of sound), such as pitch-up, buffeting, and other instabilities. This enabled reliable and routine flight of such aircraft as the century series of fighters (F-100, F-102, F-104, etc.) as well as all commercial transport aircraft from the mid-1950s to the present.＜/p＞＜p＞At the symposia honoring the 50th anniversary of the D-558-1 Skyrocket's first flight in February 1948, four D-558 pilots ー Stanley P. Butchart, Robert A. Champine, A. Scott Crossfield, and John Griffith ー plus Air Force Historian Richard Hallion offered insightful comments and meaningful anecdotes that deserved a wider audience than the few hundred people who attended. To make their recollections and related documents available to such an audience, NASA is publishing this volume.＜/p＞＜p＞The Douglas D-558-1 Skystreak and D-558-2 Skyrocket were, with the Bell XS-1, the earliest transonic research aircraft built in this country to gather data so the aviation community could understand what was happening when aircraft approached the speed of sound (roughly 741 miles per hour at sea level in dry air at 32 degrees Fahrenheit). In the early 1940s, fighter (actually, in the terms of the time, pursuit) aircraft like the P-38 Lightning were approaching these speeds in dives and either could not get out of the dives before hitting the ground or were breaking apart from the effects of compressibilityーincreased density and disturbed airflow as the speed approached that of sound and created shock waves.＜/p＞＜p＞At this time, aerodynamicists lacked accurate wind-tunnel data for the speed range from roughly Mach 0.8 to 1.2 (respectively, 0.8 and 1.2 times the speed of sound, so named in honor of Austrian physicist Ernst Mach, who ー already in the second half of the 19th century ー had discussed the speed of a body moving through a gas and how it related to the speed of sound). To overcome the limited knowledge of what was happening at these transonic speeds, people in the aeronautics community ー especially the National Advisory Committee for Aeronautics (NACA), the Army Air Forces (AAF ー Air Force after 1947), and the Navy ー agreed on the need for a research airplane with enough structural strength to withstand compressibility effects in this speed range. The AAF preferred a rocket-powered aircraft and funded the XS-1 (experimental Supersonic, later shortened to simply X), while the NACA and Navy preferred a more conservative design and pursued the D-558, with the NACA also supporting the X-1 research.＜/p＞画面が切り替わりますので、しばらくお待ち下さい。 ※ご購入は、楽天kobo商品ページからお願いします。※切り替わらない場合は、こちらをクリックして下さい。 ※このページからは注文できません。	1,022円
【中古】Introduction to Transonic Aerodynamics (Fluid Mechanics and Its Applications, 110) ブックサプライ	◇◆主にゆうメールによるポスト投函、サイズにより宅配便になります。◆梱包：完全密封のビニール包装または宅配専用パックにてお届けいたします。◆帯、封入物、及び各種コード等の特典は無い場合もございます◆◇【97467】全商品、送料無料！	16,765円
洋書 Paperback, An Introduction to Compressible Flows with Applications: Quasi-One-Dimensional Approximation and General Formulation for Subsonic, Transonic and Supersonic Flows (SpringerBriefs in Mathematics) Glomarket	* We ship internationally, so do not use a package forwarding service. We cannot ship to a package forwarding company address because of the Japanese customs regulation. If it is shipped and customs office does not let the package go, we do not make a refund. 【注意事項】 * 特に注意してください。 * ・個人ではない法人・団体名義での購入はできません。この場合税関で滅却されてもお客様負担になりますので御了承願います。・お名前にカタカナが入っている場合法人である可能性が高いため当店システムから自動保留します。カタカナで記載が必要な場合はカタカナ変わりローマ字で記載してください。・お名前またはご住所が法人・団体名義（XX株式会社等）、商店名などを含めている場合、または電話番号が個人のものではない場合、税関から法人名義でみなされますのでご注意ください。・転送サービス会社への発送もできません。この場合税関で滅却されてもお客様負担になりますので御了承願います。 * ・注文後品切れや価格変動でキャンセルされる場合がございますので予めご了承願います。・当店でご購入された商品は、原則として、「個人輸入」としての取り扱いになり、すべてニュージャージからお客様のもとへ直送されます。・ご注文後、30営業日以内(通常2~3週間)に配送手続きをいたします。配送作業完了後、2週間程度でのお届けとなります。・まれに商品入荷状況や国際情勢、運送、通関事情により、お届けが2ヶ月までかかる場合がありますのでお急ぎの場合は注文をお控えください。・個人輸入される商品は、すべてご注文者自身の「個人使用・個人消費」が前提となりますので、ご注文された商品を第三者へ譲渡・転売することは法律で禁止されております。・関税・消費税が課税される場合があります。詳細はこちらをご確認下さい。PC販売説明文	8,625円
Mathematical Aspects of Subsonic and Transonic Gas Dynamics【電子書籍】[ Lipman Bers ] 楽天Kobo電子書籍ストア	＜p＞This concise volume by a prominent mathematician offers an important survey of mathematical aspects of the theory of compressible fluids. The treatment is geared toward advanced undergraduates and graduate students in physics, applied mathematics, and engineering. Focusing on two-dimensional steady potential flows, the text eschews detailed proofs in favor of clear indications of the main ideas and descriptions of new mathematical concepts and methods that arose in connection with these chapters in fluid dynamics.＜br /＞ Starting with a general discussion of the differential equations of a compressible gas flow, the book advances to the mathematical background of subsonic flow theory. Subsequent chapters explore the behavior of a flow at infinity and methods for the determination of flows around profiles, flows in channels and with a free boundary, the mathematical background of transonic gas dynamics, and some problems in transonic flow. An extensive bibliography of 400 papers concludes the text.＜/p＞画面が切り替わりますので、しばらくお待ち下さい。 ※ご購入は、楽天kobo商品ページからお願いします。※切り替わらない場合は、こちらをクリックして下さい。 ※このページからは注文できません。	2,130円
An Introduction to Compressible Flows with Applications Quasi-One-Dimensional Approximation and General Formulation for Subsonic, Transonic and Supersonic Flows【電子書籍】[ Jos? Pontes ] 楽天Kobo電子書籍ストア	＜p＞This book offers a concise and practical survey of the principles governing compressible flows, along with selected applications.＜/p＞＜p＞It starts with derivation of the time-dependent, three-dimensional equation of compressible potential flows, and a study of weak waves, including evaluation of the sound speed in gases. The following chapter addresses quasi-one-dimensional flows, the study of normal shock waves, and flow in ducts with constant cross section subjected to friction and/or heat transfer. It also investigates the effects of friction and heat transfer in ducts with variable cross section. The chapter ends by pointing to the analogy between one-dimensional compressible flows and open channel hydraulics.＜/p＞＜p＞Further, the book discusses supersonic flows, including the study of oblique shock waves, and supersonic flows over corners and wedges. It also examines Riemann problems, numerical resolution of the wave equation, and of nonlinear hyperbolic problems, including propagation of strong waves. A subsequent chapter focuses on the small perturbation theory of subsonic, transonic and supersonic flows around slender bodies aligned or almost aligned to the uniform inflow. In particular, it explores subsonic and supersonic flows over a wavy wall. Lastly, an appendix with a short derivation of the Fluid Mechanics basic equations is included.＜/p＞＜p＞The final chapter addresses the problem of transonic flows where both subsonic and supersonic are present. Lastly, an appendix with a short derivation of the Fluid Mechanics basic equations is included.＜/p＞＜p＞Illustrated with several practical examples, this book is a valuable tool to understand the most fundamental mathematical principles of compressible flows. Graduate Mathematics, Physics and Engineering students as well as researchers with an interest in the aerospace sciences benefit from this work.＜/p＞画面が切り替わりますので、しばらくお待ち下さい。 ※ご購入は、楽天kobo商品ページからお願いします。※切り替わらない場合は、こちらをクリックして下さい。 ※このページからは注文できません。	2,721円
The Transonic Sacrifice The Mystery of Death in Life【電子書籍】[ Glen C. Cutlip ] 楽天Kobo電子書籍ストア	＜p＞There is no available information at this time. Author will provide once available.＜/p＞画面が切り替わりますので、しばらくお待ち下さい。 ※ご購入は、楽天kobo商品ページからお願いします。※切り替わらない場合は、こちらをクリックして下さい。 ※このページからは注文できません。	452円
季刊トランソニック 2 春号特集：記号かたち・楽譜【中古】ナインブリックス楽天市場店	-,全音楽譜出版社,刊行：1971年ISBN：-状態：C　ヤケ、表紙・小口経年シミ強め。※併売品のため品切れの際はご容赦ください。	3,000円
Ala Aeroelastica Attiva Migliora la manovrabilit? dell'aeromobile a velocit? transonica e supersonica【電子書籍】[ Fouad Sabry ] 楽天Kobo電子書籍ストア	＜p＞＜strong＞Cos'? l'ala aeroelastica attiva＜/strong＞＜/p＞＜p＞Il programma di sviluppo dell'X-53 Active Aeroelastic Wing (AAW) ? un progetto di ricerca americano che ? stato completato. Questo progetto ? stato realizzato congiuntamente dall'Air Force Research Laboratory (AFRL), dalla Boeing Phantom Works e dal Dryden Flight Research Center della NASA. Al Dryden Flight Research Center della NASA, la tecnologia ? stata testata in volo su un McDonnell Douglas F/A-18 Hornet modificato. La tecnologia Active Aeroelastic Wing ? una tecnologia che unisce l'aerodinamica, i controlli e la struttura di un'ala per sfruttare e regolare la torsione aeroelastica che un'ala sperimenta sotto stress dinamici e alte velocit?. L'uso di pi? controlli del bordo d'attacco e di uscita, come le "schede aerodinamiche", consente di controllare piccole quantit? di torsione aeroelastica per fornire grandi quantit? di potenza di controllo dell'ala, riducendo al contempo al minimo i carichi d'aria di manovra in condizioni di deformazione dell'ala elevata o la resistenza aerodinamica in condizioni di condizioni di basso sforzo alare. Ci? si ottiene mantenendo un equilibrio tra i due estremi delle condizioni di deformazione alare. Questa operazione ? stata la prima dimostrazione in assoluto della tecnologia AAW su larga scala.＜/p＞＜p＞＜strong＞Come ne trarrai vantaggio＜/strong＞＜/p＞＜p＞(I) Approfondimenti e convalide sul seguenti argomenti:＜/p＞＜p＞Capitolo 1: Ala aeroelastica attiva＜/p＞＜p＞Capitolo 2: Alettoni＜/p＞＜p＞Capitolo 3: Aeroelasticit?＜/p＞＜p＞Capitolo 4: Elevon＜/p＞＜p＞Capitolo 5: NASA X-43＜/p＞＜p＞Capitolo 6: Elenco di velivoli sperimentali＜/p＞＜p＞Capitolo 7: Boeing X-45＜/p＞＜p＞Capitolo 8 : Grumman X-29＜/p＞＜p＞Capitolo 9: Laboratorio di ricerca dell'aeronautica＜/p＞＜p＞Capitolo 10: Boeing X-48＜/p＞＜p＞Capitolo 11: Ascensori (aeronautica)＜/p＞＜p＞Capitolo 12: Flap (aeronautica)＜/p＞＜p＞Capitolo 13: DATCOM digitale per la stabilit? e il controllo dell'aeronautica degli Stati Uniti＜/p＞＜p＞Capitolo 14: Bracciale all'avanguardia＜/p＞＜p＞Capitolo 15: Flaperon＜/p＞＜p＞Capitolo 16: Spoileron＜/p＞＜p＞Capitolo 17: McDonnell Douglas F-15 STOL/MTD＜/p＞＜p＞Capitolo 18: Boeing X-51 Waverider＜/p＞＜p＞Capitolo 19: Ala adattabile＜/p＞＜p＞Capitolo 20: Lamella all'avanguardia＜/p＞＜p＞Capitolo 21: General Dynamics-Boeing AFTI/F-111A Aardvark＜/p＞＜p＞(II) Rispondere alle principali domande del pubblico sull'ala aeroelastica attiva Boeing x53.＜/p＞＜p＞(III) Esempi del mondo reale per l'utilizzo dell'ala aeroelastica attiva Boeing x53 in molti campi.＜/p＞＜p＞(IV) 17 appendici per spiegare, brevemente, 266 tecnologie emergenti in ciascun settore per avere una piena comprensione a 360 gradi delle tecnologie dell'ala aeroelastica attiva Boeing x53.＜/p＞＜p＞＜strong＞Chi questo Il libro ? per＜/strong＞＜/p＞＜p＞Professionisti, studenti universitari e laureati, appassionati, hobbisti e coloro che vogliono andare oltre le conoscenze o le informazioni di base per qualsiasi tipo di ala aeroelastica attiva boeing x53.＜/p＞画面が切り替わりますので、しばらくお待ち下さい。 ※ご購入は、楽天kobo商品ページからお願いします。※切り替わらない場合は、こちらをクリックして下さい。 ※このページからは注文できません。	700円
Transonics Developing a New World Consciousness【電子書籍】[ Glen C. Cutlip ] 楽天Kobo電子書籍ストア	＜p＞TRANSONICS PRESENTS AN ENIGMA IN THE NATURE OF GOD AND YOU Why is it that one believes that things have happened in the past, and that things will happen in the future, yet is unable to reconcile these two extremes with the present concepts of things?＜/p＞画面が切り替わりますので、しばらくお待ち下さい。 ※ご購入は、楽天kobo商品ページからお願いします。※切り替わらない場合は、こちらをクリックして下さい。 ※このページからは注文できません。	452円