German Development of the Swept Wing 1935–1945.

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 -- 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.

Description based on publisher supplied metadata and other sources.

Electronic reproduction. Ann Arbor, Michigan : ProQuest Ebook Central, 2024. Available via World Wide Web. Access may be limited to ProQuest Ebook Central affiliated libraries.