75 results on '"Edquist, Karl T"'
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52. Sizing and Margins Assessment of Mars Science Laboratory Aeroshell Thermal Protection System
53. Uncertainty Analysis of Mars Entry Flows over Hypersonic Inflatable Aerodynamic Decelerators
54. Supersonic Retropropulsion Computational Fluid Dynamics Validation with Langley 4×4 Foot Test Data
55. Supersonic Retropropulsion Experimental Results from NASA Ames 9×7 Foot Supersonic Wind Tunnel
56. Supersonic Retropropulsion Computational-Fluid-Dynamics Validation with Ames 9×7 Foot Test Data
57. Development of Supersonic Retropropulsion for Future Mars Entry, Descent, and Landing Systems
58. Analysis of Navier–Stokes Codes Applied to Supersonic Retropropulsion Wind-Tunnel Test
59. Mars Science Laboratory Heatshield Aerothermodynamics: Design and Reconstruction
60. Supersonic Aerodynamic Characteristics of Blunt Body Trim Tab Configurations
61. Testing of the Trim Tab Parametric Model in NASA Langley’s Unitary Plan Wind Tunnel
62. IRVE-3 Post-Flight Reconstruction
63. Modeling of Shock Tunnel Aeroheating Data on the Mars Science Laboratory Aeroshell
64. Aerodynamics for Mars Phoenix Entry Capsule
65. Overview of Entry Descent and landing investments in the NASA Exploration Technology Development Program
66. Analysis of Navier-Stokes codes applied to Supersonic Retro-Propulsion wind tunnel test
67. Mars Science Laboratory Entry Capsule Aerothermodynamics and Thermal Protection System
68. FATEPEN, a model to Predict Terminal Ballistic Penetration and Damage to Military Targets
69. Modeling of Shock Tunnel Aeroheating Data on the Mars Science Laboratory Aeroshell
70. Aeroheating Environments for a Mars Smart Lander
71. Mars Science Laboratory Experimental Aerothermodynamics with Effects of Cavities and Control Surfaces
72. Supersonic retropropulsion CFD validation with Ames Unitary Plan Wind Tunnel test data.
73. Time resolved plastic deformations in rods subjected to transverse impact
74. Transverse loading and response of long rod penetrators during high velocity plate perforation
75. Two-Dimensional Ablation and Thermal Response Analyses for Mars Science Laboratory Heat Shield.
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