Transport - Supersonic Flight. The Bigger Picture: Boom Supersonic XB-1

2020 ◽  
Vol 15 (11) ◽  
pp. 14-15
Keyword(s):  
2013 ◽  
Vol 44 (3) ◽  
pp. 405-417
Author(s):  
Anatoliy Pavlovich Mazurov ◽  
Sergey Alexandrovich Takovitsky
Keyword(s):  

Shock Waves ◽  
2015 ◽  
Vol 25 (2) ◽  
pp. 189-204
Author(s):  
W. Jiajan ◽  
R. S. M. Chue ◽  
T. Nguyen ◽  
S. C. M. Yu
Keyword(s):  

2021 ◽  
Author(s):  
Skyler M. Jacob ◽  
Johnathan Burgess ◽  
Colin Watson ◽  
Jake Compton ◽  
Gaurav Jalan ◽  
...  

1954 ◽  
Vol 58 (520) ◽  
pp. 239-245
Author(s):  
C. H. E. Warren

Before discussing the noise associated with supersonic flight, it is pertinent to restate the sources of noise at subsonic speeds.As Lilley has pointed out, noise at subsonic speeds is due to turbulence, such as occurs in jets, wakes, boundary layers, and regions of separation, and to vortices and regions of shear flow. In all these types of flow viscosity plays a predominant part, and therefore at subsonic speeds the noise of an aircraft depends very much upon the viscosity of the fluid: in an inviscid fluid, an aircraft would make no noise, because, at subsonic speeds, the pressure changes induced by its motion would be too gradual to be audible.


Author(s):  
Marcin Figat ◽  
Agnieszka Kwiek

This paper presents the results of a numerical study of the aerodynamic shape of the Rocket Plane LEX. The Rocket Plane is a main part of the Modular Airplane System – MAS; a special vehicle devoted to suborbital tourist flights. The Rocket Plane was designed for subsonic and supersonic flight conditions. Therefore, the impact of the Mach number should be considered during the aerodynamic design of the Rocket Plane. The main goal of the investigation was to determine the sensitivity of the Rocket Plane aerodynamic characteristics to the Mach number during the optimisation of the LEX geometry. The paper includes results of the optimisation process for Mach number from the range Ma = 0.5 to Ma = 2.5. These results reveal that the aerodynamic characteristics of models optimised for the subsonic and transonic regime of Mach numbers (up to Ma = 1) were also improved for the supersonic speed regime. However, in the case of models optimised for the supersonic flight regime the aerodynamic characteristics in subsonic flight regime, are inferior compared to the model before the optimisation process.


1999 ◽  
Vol 20 (1) ◽  
pp. 71-89
Author(s):  
Katrina Honeyman ◽  
David J. Starkey ◽  
Michael Bonavia ◽  
Roger Price ◽  
Peter Lyth ◽  
...  

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