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Shock Wave Technical Reports PAM 2480
[Princeton, N.J.] : Palmer Physics Laboratory, Princeton University, 195?
Walker Bleakney: Principal Investigator

Author	Title	Project No.	Series No.	Contract No.	Record No.
Taub, A.H.	Some Numerical Results on Refraction of Plane Shocks	NR061-020	PAM 2480	N6ori-105, Task II	II-A
Emrich, R.J.	Velocity Loss Measurements on Shocks in a Shock Tube	NR061-020	PAM 2480	N6ori-105, Task II	II-B
Bleakney, Walker	The Diffraction of Shock Waves Around Obstacles and the Transient Loading of Structures	NR061-020	PAM 2480	N6ori-105, Task II	II-3
Fletcher, Charles H.	The Mach Reflection of Weak Shock Waves	NR061-020	PAM 2480	N6ori-105, Task II	II-4
Stoner, Richard G. & Walker Bleakney	The Effect of Wind Variations on Sound Velocity Used in Shock Wave Measurements	NR061-020	PAM 2480	N6ori-105, Task II	II-5
White, D.R., D.K. Weimer & Walker Bleakney	The Diffraction of Shock Waves Around Obstacles and the Resulting Transient Loading of Structures	NR061-020	PAM 2480	N6ori-105, Task II	II-6
Griffith, W.C., D.K. Weimer, D.E. Brickl & Walker Bleakney	The Effect of Reynolds Number on the Diffraction of a Shock Wave	NR061-020	PAM 2480	N6ori-105, Task II	II-8
Jahn, Robert G.	Photoelastic Stress Analysis of a Shock Loaded Body	NR061-020	PAM 2480	N6ori-105, Task II	II-9
White, Donald R.	An Experimental Survey of the Mach Reflection of Shock Waves	NR061-020	PAM 2480	N6ori-105, Task II	II-10
Bleakney, Walker	Shock Loading of Rectangular Structures	NR061-020	PAM 2480	N6ori-105, Task II	II-11
Griffith, Wayland C.	Transonic Flow	NR061-020	PAM 2480	N6ori-105, Task II	II-7
White, Donald R. & David K. Weimer	A Method for Modification of the Pressure Profile in a Shock Tube	NR061-020	PAM 2480	N6ori-105, Task II	II-12
Bingham, Harry H., David K. Weimer & Wayland Griffith	The Cylinder and the Semicylinder in Subsonic Flow	NR061-020	PAM 2480	N6ori-105, Task II	II-13
Brickl, D.E. & Walker Bleakney	The Diffraction of a Shock Wave over a Three-Dimensional Object	NR061-020	PAM 2480	N6ori-105, Task II	II-14
Smith, Wesley R.	Diffraction of a Shock Wave over a Rectangular Notch	NR061-020	PAM 2480	N6ori-105, Task II	II-15
Jahn, Robert G.	The Refraction of Shock Waves at a Gaseous Interface: Regular Refraction of Weak Shocks	NR061-020	PAM 2480	N6ori-105, Task II	II-16
Griffith, Wayland C. & Walker Bleakney	Diffusion Analogy to Interaction of a Shock with a Thermal Boundary Layer	NR061-020	PAM 2480	N6ori-105, Task II	II-17
Jahn, Robert G.	The Refraction of Shock Waves at a Gaseous Interface: II. Regular Refraction of Strong Shocks	NR061-020	PAM 2480	N6ori-105, Task II	II-18
Jahn, Robert G.	The Refraction of Shock Waves at a Gaseous Interface: III. Irregular Refraction	NR061-020	PAM 2480	N6ori-105, Task II	II-19
Blackman, Vernon H.	Vibrational Relaxation in O₂ and N₂	NR061-020	PAM 2480	N6ori-105, Task II	II-20
Howard, L.N. & D.L. Matthews	On the Vortices Produced in Shock Diffraction	NR061-020	PAM 2480	N6ori-105, Task II	II-21
Bershader, D. & J. Allport	On the Laminar Boundary Layer Induced by a Travelling Shock Wave	NR061-020	PAM 2480	N6ori-105, Task II	II-22
Griffith, Wayland C. & Anne Kenny	States of partial equilibrium behind shock waves in O₂ , N₂ , CO, CO₂ , and N₂O	NR061-020	PAM 2480	N6ori-105, Task II	II-23
Niblett, G.B.F. & Anne Kenny	An Approximate Calculation of Equilibrium Conditions behind Shock Waves in the Noble Gases	NR061-020	PAM 2480	N6ori-105, Task II	II-24
Smith, W.R.	States of Partial and Complete Equilibrium Behind Shock Waves in N₂O and NO	NR061-020	PAM 2480	N6ori-105, Task II	II-25