Kubota, Toshi
- Yeung, Moon-Tai (1993) Chemical Reactions in a Scramjet Combustor and Two-Dimensional Nozzles; 10.7907/vw7e-nq49
- Yang, Joseph (1991) An analytical and computational investigation of shock-induced vortical flows with applications to supersonic combustion; 10.7907/SZQ1-YB88
- Waitz, Ian Anton (1991) An Investigation of Contoured Wall Injectors for Hypervelocity Mixing Augmentation; 10.7907/MPJS-1Q71
- Zhuang, Mei (1990) An investigation of the inviscid spatial instability of compressible mixing layers; 10.7907/650s-9t96
- Doan, Phuc The (1981) Computing the Development of Disturbances in the Blasius Boundary Layer Due to Localized Unsteady Two-Dimensional Wall Injection; 10.7907/bt7y-zn32
- Mullainathan, M. (1980) Finite-Difference Solution of Steady Two-Dimensional Boundary-Layer Equations with Heat Transfer; 10.7907/rawg-2g03
- Higuchi, Hiroshi (1977) Experimental Investigation on Axisymmetric Turbulent Wakes with Zero Momentum Defect; 10.7907/121B-VN50
- Berg, Dale Evan (1977) Surface Roughness Effects on the Hypersonic Turbulent Boundary Layer; 10.7907/2S44-JV38
- Sarohia, Virendra (1975) Experimental and Analytical Investigation of Oscillations in Flows over Cavities; 10.7907/WJC1-X942
- Rizk, Magdi Hanna (1974) Nonsteady Fluid Mechanics of Vehicles in Tubes; 10.7907/8PJF-8H92
- Ikawa, Hideo (1973) Turbulent Mixing Layer Experiment in Supersonic Flow; 10.7907/4MBK-D880
- Lee, Peter Hoong-Yee (1973) An Investigation of Collisionless Plasma Beam Interaction with a Nonhomogeneous Magnetic Field; 10.7907/XNF6-9D90
- Ramaswamy, Mathagondapally A. (1971) Experimental Investigation of the Effect of Cooling on Near Wake of Circular Cylinder at Mach Number Six; 10.7907/8ZZ8-PC49
- Sigal, Asher (1971) An Experimental Investigation of the Turbulent Boundary Layer Over a Wavy Wall; 10.7907/VK9A-XA44
- Gran, Robert Lee (1970) Step Induced Separation of a Turbulent Boundary Layer: Part I. Experiments in Supersonic Flow. Part II. A Model for Incompressible Flow in a Channel; 10.7907/XZZS-AR89
- Ko, Denny Ru-sue (1969) I. Supersonic Laminar Boundary Layer Along a Two-Dimensional Adiabatic Curved Ramp. II. Non-Linear Stability Theory for a Laminar, Incompressible Wake; 10.7907/DM2V-N712
- Victoria, Keith Jordis (1969) The Hypersonic Laminar Boundary Layer Near a Sharp Expansion Corner; 10.7907/EZX3-M918
- Chao, Chia-Chun (1968) Constant-Pressure Laminar Mixing of a Shear Layer with a Quiescent Fluid; 10.7907/8FYR-SB25
- Witte, Arvel Benjamin (1967) Part I. Experimental Investigation of an Arc-Heated Supersonic Free Jet. Part II. Analysis of One-Dimensional Isentropic Flow for Partially Ionized Argon; 10.7907/STEK-4N18
- Lewis, John Eldon (1967) Experimental Investigation of Supersonic, Laminar, Two-Dimensional, Boundary Layer Separation in a Compression Corner with and without Cooling; 10.7907/R0FB-DD20
- Batt, Richard George (1967) Experimental Investigation of Wakes Behind Two-Dimensional Slender Bodies at Mach Number Six; 10.7907/3WW3-B746
- Tyson, Thomas Janney (1967) Laminar Boundary Layers in the Neighborhood of Abrupt Spatial Disturbances; 10.7907/S72R-AM75
- Puhl, Andreas (1966) Hypersonic Boundary Layer Flow Around a Sharp Corner; 10.7907/2TPX-DD83
- Behrens, Hermann Wilhelm (1966) Flow Field and Stability of the Far Wake Behind Cylinders at Hypersonic Speeds; 10.7907/K0KH-9W58
- Herzog, Robert Theodore (1964) Nitrogen Injection into the Base Region of a Hypersonic Wake; 10.7907/J4XP-F867
- Tracy, Richard Ripley (1964) Hypersonic Flow Over a Yawed Circular Cone; 10.7907/RMWT-TH67
- McCarthy, John Francis (1962) Hypersonic Wakes; 10.7907/63NK-AG38
- Renard, Marc L. (1962) Experimental Investigation of an Arc Heater; 10.7907/SVWJ-NB92
- Kingsland, Louis (1961) Experimental Study of Helium and Argon Diffusion in the Wake of a Circular Cylinder at M = 5.8; 10.7907/1FDZ-JX04
- Anderson, David Ellsworth (1960) Investigation of Ablation of Ice Bodies in Hypersonic Flows; 10.7907/CD24-6081
- Mohlenhoff, William (1960) Experimental Study of Helium Diffusion in the Wake of a Circular Cylinder at M=5.8; 10.7907/QH2Z-TC50