Comparison of the first shock wave around the nose of three flying Oswatitsch diffusers (New Mexico shadowgraph) with the cone flow theory
By: Ph. W. Zettler-Seidel.
Contributors: U.S. Naval Ordnance Laboratory, White Oak, Md
Series: U.S. Naval Ordnance Laboratory. Mechanics Division technical note -- no. SB/Tm-18.2-3
Publisher: U.S. Naval Ordnance Laboratory
Published: 1947
Place of publication: [S.l.]
Number of pages: 11