Laderman, 1980 - Google Patents
Adverse pressure gradient effects on supersonic boundary-layer turbulenceLaderman, 1980
- Document ID
- 14546615817346785653
- Author
- Laderman A
- Publication year
- Publication venue
- AIAA Journal
External Links
Snippet
SOLUTIONS to the supersonic boundary-layer equations require accurate models to describe the turbulent transport of energy and momentum. The transport coefficients cannot be derived from first principles, but must be deduced from well-designed experimental …
- 230000000694 effects 0 title abstract description 29
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR
- G01M9/00—Aerodynamic testing; Arrangements in or on wind tunnels
- G01M9/02—Wind tunnels
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01F—MEASURING VOLUME, VOLUME FLOW, MASS FLOW OR LIQUID LEVEL; METERING BY VOLUME
- G01F1/00—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through the meter in a continuous flow
- G01F1/05—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through the meter in a continuous flow by using mechanical effects
- G01F1/34—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through the meter in a continuous flow by using mechanical effects by measuring pressure or differential pressure
- G01F1/36—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through the meter in a continuous flow by using mechanical effects by measuring pressure or differential pressure the pressure or differential pressure being created by the use of flow constriction
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR
- G01M9/00—Aerodynamic testing; Arrangements in or on wind tunnels
- G01M9/06—Measuring arrangements specially adapted for aerodynamic testing
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01F—MEASURING VOLUME, VOLUME FLOW, MASS FLOW OR LIQUID LEVEL; METERING BY VOLUME
- G01F1/00—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through the meter in a continuous flow
- G01F1/76—Devices for measuring mass flow of a fluid or a fluent solid material
- G01F1/86—Indirect mass flowmeters, e.g. measuring volume flow and density, temperature or pressure
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING; COUNTING
- G06F—ELECTRICAL DIGITAL DATA PROCESSING
- G06F17/00—Digital computing or data processing equipment or methods, specially adapted for specific functions
- G06F17/50—Computer-aided design
- G06F17/5009—Computer-aided design using simulation
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01F—MEASURING VOLUME, VOLUME FLOW, MASS FLOW OR LIQUID LEVEL; METERING BY VOLUME
- G01F1/00—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through the meter in a continuous flow
- G01F1/68—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through the meter in a continuous flow by using thermal effects
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N25/00—Investigating or analyzing materials by the use of thermal means
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
- G01P5/00—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft
- G01P5/14—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring differences of pressure in the fluid
- G01P5/16—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring differences of pressure in the fluid using Pitot tubes, e.g. Machmeter
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01K—MEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
- G01K17/00—Measuring quantity of heat
- G01K17/06—Measuring quantity of heat conveyed by flowing mediums, e.g. in heating systems e.g. the quantity of heat in a transporting medium, delivered to or consumed in an expenditure device
- G01K17/08—Measuring quantity of heat conveyed by flowing mediums, e.g. in heating systems e.g. the quantity of heat in a transporting medium, delivered to or consumed in an expenditure device based upon measurement of temperature difference or of a temperature
- G01K17/20—Measuring quantity of heat conveyed by flowing mediums, e.g. in heating systems e.g. the quantity of heat in a transporting medium, delivered to or consumed in an expenditure device based upon measurement of temperature difference or of a temperature across a radiating surface, combined with ascertainment of the heat transmission coefficient
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N33/00—Investigating or analysing materials by specific methods not covered by the preceding groups
- G01N33/44—Investigating or analysing materials by specific methods not covered by the preceding groups resins; rubber; leather
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR
- G01M3/00—Investigating fluid-tightness of structures
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Aeschliman et al. | Experimental methodology for computational fluid dynamics code validation | |
| Laderman | Adverse pressure gradient effects on supersonic boundary-layer turbulence | |
| Horstman et al. | Turbulent properties of a compressible boundary layer. | |
| Horstman et al. | Reynolds number effects on shock-wave turbulent boundary-layer interactions | |
| Holden et al. | Measurements in Regions of Low Density Laminar Shock Wave/Boundary Layer Interaction in Hypervelocity Flows and Comparison with Navier-Stokes Predictions. | |
| Wheaton et al. | Hypersonic boundary-layer instabilities due to near-critical roughness | |
| Kussoy et al. | Investigation of a three-dimensional shock wave separated turbulent boundary layer | |
| Surzhikov et al. | Study of convective heating of segmental-conical Martian descent vehicle in shock wind tunnel | |
| Anderson et al. | Experimental study of a pressure-driven, three-dimensional, turbulent boundary layer | |
| Wheaton et al. | Instability and transition due to near-critical roughness in a hypersonic laminar boundary layer | |
| Johnston et al. | A study of flush air data system calibration using numerical simulation | |
| Micol | Experimental and predicted pressure and heating distributions for aeroassist flight experiment vehicle | |
| Fischer | Experimental Laminar, Transitional, and Turbulent Boundary-layer Profiles on a Wedge at Local Mach Number 6.5 and Comparisons with Theory | |
| Rose et al. | Reynolds-shear-stress measurements in a compressible boundary layer within a shock-wave-induced adverse pressure gradient | |
| Miller III et al. | Real-air data reduction procedures based on flow parameters measured in the test section of supersonic and hypersonic facilities | |
| Laganelli et al. | The effects of mass transfer and angle of attack on hypersonic turbulent boundary layer characteristics | |
| Fiore et al. | Calibration of a boundary layer fence technique for surface shear stress measurements in a compressible flow field | |
| Erickson | Overview of selected measurement techniques for aerodynamics testing in the NASA Langley Unitary Plan Wind Tunnel | |
| GREGOREK | Viscous effects on blunt cones at hypersonic speeds | |
| Hozumi et al. | Investigation of hypersonic compression ramp heating at high angles of attack | |
| Hedlund et al. | Aerodynamic and aerothermal instrumentation-Measurement uncertainty in the NSWC Hypervelocity Wind Tunnel No. 9 | |
| Beresh et al. | Measurement of Experimental Boundary Conditions for CFD Validation of a Supersonic Jet in Transonic Crossflow | |
| Gaisbauer et al. | Shock/Turbulent Boundary Layer Interaction on a Double Ramp Configuration-Experiments and Computations | |
| Dye | An experimental and computational investigation of the flowfield about an Aeroassisted Space Transportation Vehicle at Mach 10 | |
| PATE | Induced boundary-layer transition at supersonic speeds-Combined effects of roughness and free-stream disturbances |