Add to ORKGThe sonic boom flight test program conducted at Jackass Flats, Nevada, during the summer and fall of...
The sonic boom is one of the most severe problems confronting the advancement of high-speed air tran...
Wind tunnel investigation of delta-wing-body combination sonic boom at Mach 1.41 and 2.0
Numerical method for calculating near field sonic room pressure signatures and application to high s...
This paper first describes the numerical simulation and shape optimization of the Lockheed SEEB-ALR ...
In this paper a simple approach aimed to the definition of a supersonic configuration optimized in t...
Development of near-field method for determining supersonic flow properties about bodies of revoluti...
Wind tunnel tests were conducted to determine the characteristics of sonic booms. A theoretical exam...
Aircraft sonic boom characteristics predicted from near field data obtained in wind tunne
Estimated supersonic flow field shock waves and sonic boom effects for cones and axisymmetric bodie
The analysis of the 14 low-altitude transonic flights showed that the prevailing meteorological cons...
A 3-D parabolized Navier-Stokes (PNS) code was used to calculate the supersonic overpressures from t...
Comparison of measured and calculated sonic boom ground patterns due to aircraft maneuver
A second-order theory for supersonic flow past slender bodies is presented. Through the introduction...
Wind tunnel measurements on effect of slender body shape on sonic boom pressure distribution
The sonic boom flight test program conducted at Jackass Flats, Nevada, during the summer and fall of...
The sonic boom is one of the most severe problems confronting the advancement of high-speed air tran...
Wind tunnel investigation of delta-wing-body combination sonic boom at Mach 1.41 and 2.0
Numerical method for calculating near field sonic room pressure signatures and application to high s...
This paper first describes the numerical simulation and shape optimization of the Lockheed SEEB-ALR ...
In this paper a simple approach aimed to the definition of a supersonic configuration optimized in t...
Development of near-field method for determining supersonic flow properties about bodies of revoluti...
Wind tunnel tests were conducted to determine the characteristics of sonic booms. A theoretical exam...
Aircraft sonic boom characteristics predicted from near field data obtained in wind tunne
Estimated supersonic flow field shock waves and sonic boom effects for cones and axisymmetric bodie
The analysis of the 14 low-altitude transonic flights showed that the prevailing meteorological cons...
A 3-D parabolized Navier-Stokes (PNS) code was used to calculate the supersonic overpressures from t...
Comparison of measured and calculated sonic boom ground patterns due to aircraft maneuver
A second-order theory for supersonic flow past slender bodies is presented. Through the introduction...
Wind tunnel measurements on effect of slender body shape on sonic boom pressure distribution
The sonic boom flight test program conducted at Jackass Flats, Nevada, during the summer and fall of...
The sonic boom is one of the most severe problems confronting the advancement of high-speed air tran...
Wind tunnel investigation of delta-wing-body combination sonic boom at Mach 1.41 and 2.0