High Speed Problems of Aircraft and Experimental Methods -

High Speed Problems of Aircraft and Experimental Methods

Allen F. Donovan (Herausgeber)

Buch | Softcover
1024 Seiten
2015
Princeton University Press (Verlag)
978-0-691-62560-7 (ISBN)
198,25 inkl. MwSt
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.

*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

Erscheinungsdatum
Reihe/Serie Princeton Legacy Library
Verlagsort New Jersey
Sprache englisch
Maße 152 x 235 mm
Gewicht 1389 g
Themenwelt Naturwissenschaften Physik / Astronomie
Technik Fahrzeugbau / Schiffbau
Technik Luft- / Raumfahrttechnik
ISBN-10 0-691-62560-3 / 0691625603
ISBN-13 978-0-691-62560-7 / 9780691625607
Zustand Neuware
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