Longitudinal stability and control of a Mach 10 “scramjet” glider

Mudford, Neil R. and Boyce, Russell R. (2005). Longitudinal stability and control of a Mach 10 “scramjet” glider. In: A Collection of Technical Papers - 13th AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference, Capua, Italy, (1827-1841). 16-20 May 2005.


Author Mudford, Neil R.
Boyce, Russell R.
Title of paper Longitudinal stability and control of a Mach 10 “scramjet” glider
Conference name AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference
Conference location Capua, Italy
Conference dates 16-20 May 2005
Convener American Institute of Aeronautics and Astronautics
Proceedings title A Collection of Technical Papers - 13th AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference
Journal name A Collection of Technical Papers - 13th AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference
Place of Publication Reston, VA
Publisher American Institute of Aeronautics and Astronautics
Publication Year 2005
Sub-type Fully published paper
ISBN 1563477297
9781563477294
Volume 3
Start page 1827
End page 1841
Total pages 15
Language eng
Abstract/Summary Results and analysis are reported of numerically intensive computations of inviscid flow around and through a two-dimensional version of a scramjet-like glider with an inward turning flowpath. Flows for sharp and blunt leading edges are compared and contrasted. Attention is focused on the longitudinal static stability of the craft. Detailed examination of the internal flow reveals pressure field shifts as the origin of the highly non-linear behavior of the pitching moment coefficient with angle of attack around the trim condition. The effect of the elevators is then examined
Subjects 090107 Hypersonic Propulsion and Hypersonic Aerodynamics
Q-Index Code E1
Institutional Status Non-UQ
Additional Notes AIAA 2005-3408

 
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