Tests on thrust augmentors for jet propulsion /

This series of tests was undertaken to determine how much the reaction thrust of a jet could be increased by the use of thrust augmentors and thus to give some indication as to the feasibility of jet propulsion for airplanes. The tests were made during the first part of 1927 at the Langley Memorial...

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Bibliographic Details
Main Author: Jacobs, Eastman N (Eastman Nixon), 1902-1987
Corporate Author: United States National Advisory Committee for Aeronautics
Other Authors: Shoemaker, James M
Format: Government Document Book
Language:English
Published: Washington D.C. : National Advisory Committee for Aeronautics, 1932
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 431
Subjects:
Description
Summary:This series of tests was undertaken to determine how much the reaction thrust of a jet could be increased by the use of thrust augmentors and thus to give some indication as to the feasibility of jet propulsion for airplanes. The tests were made during the first part of 1927 at the Langley Memorial Aeronautical Laboratory. A compressed air jet was used in connection with a series of annular guides surrounding the jet to act as thrust augmentors. The results show that, although it is possible to increase the thrust of a jet, the increase is not large enough to affect greatly the status of the problems of the application of jet propulsion to airplanes
Item Description:NACA TN no. 431
"September, 1932."
Physical Description:5, [3] p. : ill. ; 27 cm
Bibliography:Includes bibliographical references