E-Book, Englisch, Band 2421, 1024 Seiten
Reihe: Princeton Legacy Library
E-Book, Englisch, Band 2421, 1024 Seiten
Reihe: Princeton Legacy Library
ISBN: 978-1-4008-7503-0
Verlag: De Gruyter
Format: PDF
Kopierschutz: Adobe DRM (»Systemvoraussetzungen)
Autoren/Hrsg.
Weitere Infos & Material
Frontmatter, pg. i
FOREWORD, pg. v
PREFACE, pg. vii
CONTENTS, pg. ix
SECTION A. METHODS OF PERFORMANCE CALCULATION AT HIGH SPEED, pg. 3
SECTION B. STABILITY AND CONTROL OF HIGH SPEED AIRCRAFT, pg. 57
SECTION C. AERO ELASTICITY AND FLUTTER, pg. 161
SECTION D. PRINCIPLES OF MODEL TESTING, pg. 427
SECTION E. INTRODUCTORY DISCUSSION OF HIGH SPEED TEST TECHNIQUES, pg. 454
SECTION F. TRANSONIC WIND TUNNELS, pg. 460
SECTION G. SUPERSONIC TUNNELS, pg. 491
SECTION H. HYPERSONIC EXPERIMENTAL FACILITIES, pg. 533
SECTION I. LOW DENSITY WIND TUNNELS, pg. 576
SECTION J. THE SHOCK TUBE, pg. 596
SECTION K. WIND TUNNEL MEASUREMENTS, pg. 648
SECTION L. OBJECTIVES OF FREE FLIGHT RESEARCH, pg. 771
SECTION M. INSTRUMENTED MODELS IN FREE FLIGHT, pg. 775
SECTION N. PILOTED AIRCRAFT TESTING, pg. 833
SECTION O. FREE FLIGHT RANGE METHODS, pg. 905
INDEX, pg. 963