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book: High Speed Problems of Aircraft and Experimental Methods
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High Speed Problems of Aircraft and Experimental Methods

  • Edited by: Allen F. Donovan
Language: English
Published/Copyright: 1961
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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.


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PART ONE. HIGH SPEED PROBLEMS OF AIRCRAFT

I. L. Ashkenas
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3

Clarence L. Gillis and Thomas A. Toll
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57

Alexander H. Flax
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161
PART TWO. WIND TUNNEL TECHNIQUES

Albert E. Von Doenhoff
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427

Frank E. Goddard
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454

Josiah E. Smith
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460

Frank E. Goddard
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491

Henry T. Nagamatsu
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533

E. D. Kane, G. J. Maslach and Samuel A. Schaaf
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576

Walker Bleakney and R. J. Emrich
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596

H. Julian Allen, J. H. Spiegel, John Dimeff, Benjamin H. Beam, Jackson R. Stalder and Alvin Seiff
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648
PART THREE. FREE FLIGHT TECHNIQUES

Robert R. Gilruth
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771

Joseph A. Shortal and William J. O'Sullivan
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775

Frederick J. Bailey, John A. Zalovcik, William H. Phillips and Wilber B. Huston
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833

A. C. Charters
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Publishing information
Pages and Images/Illustrations in book
eBook published on:
December 8, 2015
eBook ISBN:
9781400875030
Pages and Images/Illustrations in book
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1024
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