2 research outputs found
Technical Literature Digest
- Author
- Aerodynamic Heat Transfer Measurement
- Aeronautical Sciences Progress
- Aerosols The Physical
- Airborne Missiles Underwater Launching
- Airborne Missiles Underwater Launching
- Airspeed Tables
- Arc Positive An Experimental
- Atomic
- Base On
- Charged Interaction
- Chemistry Temperature
- Diffuser Effects
- Dissociated Air Transport Properties
- Dissociation The Effect
- Distribution Pressure
- Distributions Approximate Temperature
- Electrically Conducting Fluid Heat Transfer
- Enthalpy Approximation
- Equilibrium Boundary Radiation Emission
- Equilibrium One-Dimensional Steady An Approximate
- Exact Some
- External Hypersonic Flows Chemical Effects
- Film An Approximate
- Flow Fields About Some A Study
- Free Shear-Layer Instability Some Aspects
- Free-Flight Supersonic
- Heat High Temperature
- Heat Transfer Boundary Layer
- Heat Transfer Local Aerodynamic
- Heat Transfer Similarity Modeling Technique
- Hemisphere Pressure Distributions
- Hydroand The Basic
- Hypersonic Flow Blunt Body
- Hypersonic Flows Axisymmetric Nozzles
- Hypersonic Rarefied Gas Flow A Kinetic Model
- Hypersonic Theoretical Prediction
- In-Flight Acoustic Ground
- Individual Gas Bubbles Mass Transfer
- Infrared Study
- Jet Laminar
- Kinetic On
- Laminar A Theory
- Layer Interaction Shock-Boundary
- Leading
- Lenticular-Shaped Reentry Landing Characteristics
- Magnetic Field The Interaction
- Magnetized Sphere Moving Slip Flow
- Materials Research Summary
- Measure Heat Transfer An Experimental
- Mixing Length Applicability
- Momentum Simultaneous Transfer
- Nonequilibrium Exact Solutions
- Nonisothermal Plasma Without Collisions Magnetohydrodynamics
- Nonstationary The
- Number Some Reynolds
- On
- Oscillation The
- Partially Ionized Hydrogen The Equation
- Plane Dissociation Relaxation
- Plasma Excitation
- Polyatomic Gas Heat Conduction
- Preliminary Description
- Pressure
- Radiant Heat Aerodynamic
- Reattachment Heat Transfer
- Recombination The Effect
- Research Objectives Dyna Soar
- Research Program The
- Sandia High-Altitude Sampler Design
- Shock Tube Plasma Studies
- Shock Tunnel Development Summary
- Shock Tunnel Development Summary
- Shock-Layer Hypersonic
- Similar On
- Stagnation-Point A Comparison
- Stagnation-Point Boundary The
- Structure Shock Layer
- Supersonic Flow Effect
- Supersonic Shear Flow Boundary Layer
- Surface Preparation Effect
- Table Compressible Flow
- Temperature Recovery
- Tensor Some Effects
- Thermodynamic Conditions Behind Reflected Hydrodynamic
- Thermodynamic Functions Ideal Gas
- Thermodynamic Tables
- Transfer Between Nongray Parallel Radiant Heat
- Transition Layer Structure
- Turbulent On
- Unit Reynolds Number Effects
- Wings Recent Hypersonic
- Publication venue
- 'American Institute of Aeronautics and Astronautics (AIAA)'
- Publication date
- Field of study
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