E-Book, Englisch, 1024 Seiten
Reihe: Princeton Legacy Library
Donovan High Speed Problems of Aircraft and Experimental Methods
1. Auflage 2016
ISBN: 978-1-4008-7503-0
Verlag: De Gruyter
Format: PDF
Kopierschutz: 1 - PDF Watermark
E-Book, Englisch, 1024 Seiten
Reihe: Princeton Legacy Library
ISBN: 978-1-4008-7503-0
Verlag: De Gruyter
Format: PDF
Kopierschutz: 1 - PDF Watermark
Volume VIII of the High Speed Aerodynamics and Jet Propulsion series. This volume includes: performance calculation at high speed; stability and control of high speed aircraft; aeroelasticity and flutter; model testing; transonic wind tunnels; supersonic tunnels; hypersonic experimental facilities; low density wind tunnels; shock tube; wind tunnel measurements; instrumented models in free flight; piloted aircraft testing; free flight range methods.
Originally published in 1961.
The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.
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
