LEADER 04329nam 2200601 a 450 001 9910970909503321 005 20251117094610.0 010 $a1-60086-755-3 010 $a1-60086-754-5 035 $a(CKB)2550000000072829 035 $a(EBL)3111482 035 $a(SSID)ssj0000551359 035 $a(PQKBManifestationID)12204513 035 $a(PQKBTitleCode)TC0000551359 035 $a(PQKBWorkID)10525413 035 $a(PQKB)11194479 035 $a(MiAaPQ)EBC3111482 035 $a(Au-PeEL)EBL3111482 035 $a(CaPaEBR)ebr10516535 035 $a(OCoLC)922978775 035 $a(BIP)30979605 035 $a(EXLCZ)992550000000072829 100 $a20100601d2010 uy 0 101 0 $aeng 135 $aur|n|---||||| 181 $ctxt 182 $cc 183 $acr 200 10$aGerman development of the swept wing $e1935-1945 /$fedited by Hans-Ulrich Meier ; with contributions from Burghard Ciesla ... [et al.] ; translated by Egon Stanewsky 205 $a1st ed. 210 $aReston, Va. $cAmerican Institute of Aeronautics and Astronautics in cooperation with the Deutsche Gesellschaft fu?r Luft- und Raumfahrt, Lilienthal-Oberth$dc2010 215 $a1 online resource (768 p.) 225 1 $aLibrary of flight 300 $aDescription based upon print version of record. 311 08$a1-60086-714-6 320 $aIncludes bibliographical references and index. 327 $a""COVER""; ""TITLE""; ""COPYRIGHT""; ""FOREWORD""; ""A NOTE FROM THE SERIES EDITOR""; ""CONTENTS""; ""PREFACE TO THE ENGLISH-LANGUAGE EDITION""; ""PREFACE TO THE GERMAN EDITION""; ""ACKNOWLEDGMENTS""; ""CHAPTER 1: HISTORIC REVIEW OF THE DEVELOPMENT OF HIGH-SPEED AERODYNAMICS""; ""CHAPTER 2: HIGH-SPEED FLIGHT AND ITS AERODYNAMIC AND GASDYNAMIC CHALLENGES""; ""CHAPTER 3: DEVELOPMENT OF GERMAN TURBOJET ENGINES UP TO PRODUCTION READINESS""; ""CHAPTER 4: AEROELASTICITY PROBLEMS IN COMPRESSIBLE SUBSONIC AND TRANSONIC FLOW""; ""CHAPTER 5: EFFECT OF HIGH MACH NUMBERS ON HIGH-SPEED AIRCRAFT"" 327 $a""CHAPTER 6: EXPERIENCE GAINED DURING DEVELOPMENT AND TESTING OF THE FIRST SWEPT-WING JET AIRCRAFT""""CHAPTER 7: SPECIAL FEATURES OF ANTIAIRCRAFT ROCKETS WITH SWEPT OR LOW-ASPECT-RATIO WINGS""; ""CHAPTER 8: TRANSFER OF GERMAN HIGH-SPEED AERODYNAMICS AFTER 1945""; ""APPENDIX A: ABBREVIATIONS AND ACRONYMS""; ""APPENDIX B: ENGLISH SPELLING OF EUROPEAN TOWNS AND COUNTRIES""; ""APPENDIX C: SOURCES OF ORIGINAL REPORTS""; ""INDEX""; ""CONTRIBUTING AUTHORS""; ""SUPPORTING MATERIALS"" 330 $aThis book is a translated edition of Die Pfeilfl elentwicklung in Deutschland bis 1945. The history of the development of the swept wing has been described several times during the last fifty years. But there has been no detailed description of how the original idea of the swept wing was developed into the reality that enabled highspeed flight. Together with six co-authors, Hans-Ulrich Meier investigated domestic and foreign libraries and archives to locate important original documents, including previously unavailable materials, to assess scientific and technical progress in using the swept wing in high-speed aircraft and missile projects between 1935 and 1945 in Germany. The book addresses the problems and questions concerning test and measurement techniques, aerodynamics, gas dynamics, and aeroelasticity, and experience gained in developing and testing the first jet aircraft and artillery rockets with swept wings and low aspect ratio wings. Because jet engine developments in Germany during this time period have been thoroughly documented elsewhere, only solutions concerning engine integration, engine intakes, and compressor development are presented here.The book concludes with selected examples of how the Allies utilized German knowledge. 410 0$aLibrary of flight. 606 $aAirplanes$xWings, Swept-back$xResearch$zGermany$xHistory$y20th century 615 0$aAirplanes$xWings, Swept-back$xResearch$xHistory 676 $a629.134/32 701 $aMeier$b H. U$g(Hans Ulrich)$01871922 701 $aCiesla$b Burghard$01871923 701 $aStanewsky$b E$018669 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910970909503321 996 $aGerman development of the swept wing$94480919 997 $aUNINA