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Diffraction of a plane wave by a three-dimensional cornerBy the superposition of the conical solution for the diffraction of a plane pulse by a three dimensional corner, the solution for a general incident plane wave is constructed. A numerical program is presented for the computation of the pressure distribution on the surface due to an incident plane wave of any wave form and at any incident angle. Numerical examples are presented to show the pressure signature at several points on the surface due to incident wave with a front shock wave, two shock waves in succession, or a compression wave with same peak pressure. The examples show that when the distance of a point on the surface from the edges or the vertex is comparable to the distance for the front pressure raise to reach the maximum, the peak pressure at that point can be much less than that given by a regular reflection, because the diffracted wave front arrives at that point prior to the arrival of the peak incident wave.
Document ID
19720006654
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ting, L.
(New York Univ. New York, NY, United States)
Kung, F.
(New York Univ. New York, NY, United States)
Date Acquired
August 6, 2013
Publication Date
May 1, 1971
Subject Category
Fluid Mechanics
Report/Patent Number
NYU-AA-70-28
NASA-CR-126482
Report Number: NYU-AA-70-28
Report Number: NASA-CR-126482
Accession Number
72N14303
Funding Number(s)
CONTRACT_GRANT: NGL-33-016-119
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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