2 research outputs found
Technical Literature Digest
- Author
- A
- A
- A
- Absolute Bremsstrahlung Numerical Calculation
- Advancing Characteristics Oscillations
- Aerospace Electromagnetic
- Air Dissociation Effects
- Air Jet Spectrographic Temperature
- Air Solubility
- al Arc Flexure
- An
- Attainment Research Directed
- Automation Magnetic Elements
- Axisymmetric Jet Design
- Bodies Streamlined Conical
- Boundary An Inviscid
- Carbon A Study
- Chemical Rapid
- Chemical Reaction Rates Variational Theory
- Chemical Reaction Rates Variational Theory
- Chemical Studies
- Cloud High Altitude
- Corrugated Diaphragms Bending
- Cylindrical Symmetry Analytical Solution
- del Research Basic Principles
- Designed The Noise
- Different Gases Laminar Mixing
- Doppler Effect Determination
- Droplets Theory
- During Complex Stress Histories Fatigue Damage
- Dynamics Plasma
- Electric Signals Pulse Amplification
- Electrical Thermodynamic
- Electrode The Effects
- Electromagnetic Penetration
- Energy Losses Charged Particle
- Environmental Extremes Materials
- Equilibrium
- Fast Ionization Investigation
- Fine Wire Design
- Flat Oval Bourdon Tubes Test
- Flow Channel
- Fuel Types The Effect
- General Some
- Glassy A Theory
- Guided Microwaves Plasma Acceleration
- Have Space Potential Optical Systems
- Heat On Ablating
- High Energy Oxidizers Handling
- High Performance Mechanical Properties
- High Temperature Flames Temple Studies
- High Temperatures Thermal Degradation
- Hightemperature Application New Shielding
- Honeycomb Properties
- Hydrodynamic Viscosity
- Hydrogen Rocket Chemical Nonequilibrium
- Hydrogen-Oxygen System Mollier Diagrams
- Hypersonic Environment Sublimation
- Hypersonic Shock Tunnel The
- Idealdissociating Gas Theory
- Imperfect Gas Hypersonic Flow
- Interferometry Streak
- Internal Stabilization Effects
- Internal The Effect
- Ionization A Simple Method
- Jets On Axisymmetrical
- Laboratory Data Transcription
- Laboratory Wire Strain Allegany Ballistics
- le Rocket Cases Titanium Provides
- Liquidfuel Rocket Combustion A
- Low Temperatures Thermodynamic Properties
- Magnetohydrodynamic A Study
- Magnetohydrodynamic Channel Flow End Effects
- Magnetohydrodynamic Shock Structure
- Magnetohydrodynamic Studies An Arc
- Magnetohydrostatic Equilibrium
- Many New Propellant Possibilities Fluorine Compounds
- Materials Some Factors
- Maximum Attainable On
- Meet Improved Plastics
- Missile Test Programs Television Telemeter
- Missiles Thermal Protection Paint Gives
- Molecular Comparison
- Molecular Gas Absorptivities Relations
- Nearly Linear Systems A Theory
- Nickel Stress Rupture
- Normal NMR
- Nozzle Admittance Substantiation
- Ohm's The Generalized
- Parameter Comparison
- Parametric Performance
- Partially Ionized Gases Transport Property
- Partially Ionized The Performance
- Phase Shifter Paves New Ferrite
- Polytetrafluoroethylene Pyrolysis The Mechanism
- Pozin On Increasing
- Predicting Laminar Heat Methods
- Pressure Electrical
- Probed Radio's Blackout
- Processes Ceramic Fabrication
- Processes Metal Combustion
- Production The
- Propulsion System Components Acoustic Impedance
- Prototype Camera Description
- Pulse A System
- Radio Long Range
- Random Signal Fluctuations
- Rapidly Varying Measurement
- Refractory Hard Metals Properties
- Regimes Magnetogasdynamic Flow
- Regimes Magnetogasdynamic Flow
- Rocket Engines Vaporization
- Rockets Materials
- Separated Flows Heat Transfer
- Shock Experimental Studies
- Shock Experimental Studies
- Shock Front Theory
- Shock Hugoniots Calculation
- Shock Tube Microwave Investigation
- Shock Wave Mach Waves
- Small The Wave
- Solid Propellant Search Esso Accelerates
- Some
- Sooty Flames Temperature Distribution
- Sound Field Produced Theoretical Investigation
- Space Communications Designing
- Space Simulating
- Space Vehicles Experimental Observation
- Spark An Experimental
- Spark The Electric
- Specific Heat Compressible Flow
- Spectra Flame
- Stagnation Ablation
- State of the Art
- Steady An Investigation
- Strongly The Circulation
- Structural Design Beryllium Applications
- Supersonic Gas Some Further
- Survey
- Teflon High Temperature
- Temperature Distribution Analysis
- Theoretical Flow Use
- Thermal Properties Symposium
- Thermal Survey
- Thickness Shock Front
- Thin Solid Body Motion
- Titaniumalloy Sheet Tensile Properties
- Transfer Heat
- Transfer Heat
- Transient Water Flow Phase Research
- Use
- Wave LCAO
- Wave Magnetohydrodynamic Shock
- Wings Useful Interference
- Publication venue
- 'American Institute of Aeronautics and Astronautics (AIAA)'
- Publication date
- Field of study
Full text linkTechnical 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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