Preliminary Investigation at Supersonic Speeds of Triangular and Sweptback Wings
Preliminary Investigation at Supersonic Speeds of Triangular and Sweptback Wings

Author: Macon C. Ellis

Publisher:

Published: 1949

Total Pages: 44

ISBN-13:

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Results from a supersonic wind-tunnel investigation of a series of thin triangular and sweptback wings are presented. The triangular wing series consisted of eight triangular wings of vertex angles such that a range of leading-edge postions both inside and outside the Mach cone at the test Mach numbers of 1.43 and 1.71 was obtained. The three swept wings had angles of sweep at 45, 55, and 63 degrees and were tested at a Mach number of 1.43.

High Speed Wing Theory
High Speed Wing Theory

Author: Doris Cohen

Publisher: Princeton University Press

Published: 2015-12-08

Total Pages: 251

ISBN-13: 1400874947

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Part of the Princeton Aeronautical Paperback series designed to bring to students and research engineers outstanding portions of the twelve-volume High Speed Aerodynamics and Jet Propulsion series. These books have been prepared by direct reproduction of the text from the original series and no attempt has been made to provide introductory material or to eliminate cross reference to other portions of the original volumes. Originally published in 1960. 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.

Aerodynamic Components of Aircraft at High Speeds
Aerodynamic Components of Aircraft at High Speeds

Author: Allen F. Donovan

Publisher: Princeton University Press

Published: 2015-12-08

Total Pages: 863

ISBN-13: 1400879906

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Volume VII of the High Speed Aerodynamics and Jet Propulsion series. It deals with applications to specific components of the complete aircraft. Sections of the volume include: aerodynamics of wings at high speed, aerodynamics of bodies at high speed, interaction problems, propellers at high speed, diffusers and nozzles, and nonsteady wing characteristics. Originally published in 1957. 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.

The Calculation of Downwash Behind Supersonic Wings with an Application to Triangular Plan Forms
The Calculation of Downwash Behind Supersonic Wings with an Application to Triangular Plan Forms

Author: Maxwell Alfred Heaslet

Publisher:

Published: 1948

Total Pages: 52

ISBN-13:

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A method is developed, consistent with the assumptions of small perturbation theory, which provides a means of determining for a known load distribution, the downwash behind a wing in supersonic flow. THe analysis is based upon the use of supersonic doublets which are distributed over the plan form and wake of the wing in a manner determined from the wing loading.

Investigation of Bonding Between Metals and Ceramics
Investigation of Bonding Between Metals and Ceramics

Author: H. J. Hamjian

Publisher:

Published: 1949

Total Pages: 696

ISBN-13:

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The experiments conducted with boron carbide and each of four metals showed that nickel, cobalt, and iron formed a bonding zone between the metal and the ceramic and that chromium showed satisfactory physical wetting characteristics on the ceramic.