Design Development Strategies and Technology Integration for Supersonic Aircraft of Low Perceived Sonic Boom

2003 ◽  
Author(s):  
Peter Hartwich ◽  
Billy Burroughs ◽  
James Herzberg ◽  
Curt Wiler
Keyword(s):  
Technology Integration ◽  
Development Strategies ◽  
Sonic Boom ◽  
Design Development ◽  
Supersonic Aircraft

Radiotheranostics with radiolanthanides: Design, development strategies, and medical applications

2019 ◽  
Vol 383 ◽  
pp. 104-131 ◽  
Author(s):  
Kenji Mishiro ◽  
Hirofumi Hanaoka ◽  
Aiko Yamaguchi ◽  
Kazuma Ogawa
Keyword(s):  
Development Strategies ◽  
Medical Applications ◽  
Design Development

Meteorological Parameters Affecting Supersonic Transport Operations

1967 ◽  
Vol 20 (1) ◽  
pp. 53-63 ◽  
Author(s):  
Richard Scherhag ◽  
Gunter Warnecke ◽  
Werner Wehry
Keyword(s):  
Working Group ◽  
Meteorological Parameters ◽  
Sonic Boom ◽  
Atmospheric Ozone ◽  
Atmospheric Conditions ◽  
Atmospheric Parameters ◽  
Free Atmosphere ◽  
Supersonic Transport ◽  
Supersonic Aircraft ◽  
Initial Task

In 1965, following the Eastbourne Conference, the British, French and German Institutes of Navigation formed a Working Group to make a study of the environment in which the supersonic transport will operate and of its implications for the navigation of such aircraft. The Group's initial task has been one of education, largely through discussion of a series of papers submitted to it. Some of the papers considered have already been published in the Journal (Vol. 19) and a further selection is published below. Table I was contributed by Mr. G. E. Beck. The illustrations to these papers have not all been reproduced.1. Atmospheric Conditions. It will be useful to distinguish between different kinds of atmospheric influences on supersonic aircraft operations. They may be classed as follows:(a) Sporadic effects near the ground(b) Sporadic effects in the free atmosphere(c) Effects on sonic boom(d) Effects of atmospheric ozone(e) Permanently effective atmospheric parameters, such as temperature, density and wind.

Reduction of the sonic boom level in supersonic aircraft flight by the method of surface cooling

2013 ◽  
Vol 20 (6) ◽  
pp. 669-678 ◽  
Author(s):  
V. M. Fomin ◽  
V. F. Chirkashenko ◽  
V. F. Volkov ◽  
A. M. Kharitonov
Keyword(s):  
Sonic Boom ◽  
Surface Cooling ◽  
Supersonic Aircraft ◽  
Aircraft Flight

scholarly journals Research of a High Thrust-to-Weight Ratio Small Turbofan Engine

1997 ◽  
Author(s):  
Masahiro Akagi ◽  
Masashi Shinomiya ◽  
Junichi Sakaki ◽  
Shunji Sugai
Keyword(s):  
Research And Development ◽  
Weight Ratio ◽  
Development Program ◽  
Engine Test ◽  
Test Results ◽  
Design Development ◽  
Turbofan Engine ◽  
Technical Research ◽  
Supersonic Aircraft ◽  
High Thrust

The 3rd Research Center of the Technical Research and Development Institute (TRDI) of Japan Defense Agency (JDA) and Ishikawajima-Harima Heavy Industries Co., Ltd. (IHI) developed and tested the demonstrator of a high thrust-to-weight ratio small turbofan engine with an afterburner called “XF3-400”, the purpose of which is to establish engine technologies for the future supersonic aircraft for JDA. The development program started in 1981 and the first engine test was carried out in 1992. All the engine tests planned completed in March 1995 successfully. This paper reports the design, development and test results of the XF3-400 engine above.

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