,
Teaching Resource from CaltechDATA
- Parziale, Nicholaus J. (2013) Slender-Body
Hypervelocity Boundary-Layer Instability; 10.7907/KZJ1-Y009
- Ponchaut, Nicolas Frederic (2005) Part
I: 3DPTV: Advances and Error Analysis. Part II: Extension of Guderley's
Solution for Converging Shock Waves; 10.7907/09ZH-9M66
- Belanger, Jacques (1993) Studies
of mixing and combustion in hypervelocity flows with hot hydrogen
injection; 10.7907/012K-GE91
- Mouton, Christopher Andre (2007) Transition
Between Regular Reflection and Mach Reflection in the Dual-Solution
Domain; 10.7907/TEA0-Q468
- Germain, Patrick (1994) The
boundary layer on a sharp cone in high-enthalpy flow; 10.7907/hfje-z896
- Cummings, Eric Bryant (1995) Laser-Induced
Thermal Ccoustics; 10.7907/p7mb-d967
- Sanderson, Simon Ralph (1995) Shock
wave interaction in hypervelocity flow; 10.7907/3GPK-5G29
- Rasheed, Adam (2001) Passive
Hypervelocity Boundary Layer Control Using an Ultrasonically Absorptive
Surface; 10.7907/EFZZ-X764
- Laurence, Stuart Jon (2006) Proximal
Bodies in Hypersonic Flow; 10.7907/VZJV-KJ48
- Leyva, Ivett A. (1999) Shock
detachment process on cones in hypervelocity flows; 10.7907/62TN-GA26
- Adam, Philippe H. (1997) Enthalpy
Effects on Hypervelocity Boundary Layers; 10.7907/YF0K-HK91
- Wen, Chihyung (1994) Hypervelocity
flow over spheres; 10.7907/5DDV-GW34
- Schlamp, Stefan (2000) Laser-induced
thermal acoustic velocimetry; 10.7907/skm0-tk82
- Kumar, Sanjay (2003) An
Experimental Investigation of Richtmyer-Meshkov Instability; 10.7907/NKDR-TT39
- Davis, Jean-Paul (1999) High-enthalpy
shock/boundary-layer interaction on a double wedge; 10.7907/4C98-MN23
- Bridges, David Henry (1993) Tip
effects on the vortex wake of an axisymmetric body at angle of
attack; 10.7907/DZ4H-M010
- Lemieux, Patrick (1999) The
instability of shear layers produced by curved shocks; 10.7907/V9R0-JD15
- Togami, Kenji (1993) Hypervelocity
dissociating flow over a spherically blunted cone; 10.7907/kewn-2m49
- Rousset, Bernard (1995) Calibration
and Study of the Contoured Nozzle of the T5 Free-Piston Hypervelocity
Shock Tunnel; 10.7907/A82S-0J92