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Aerodynamics, Transonic
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The concept ** Aerodynamics, Transonic** represents the subject, aboutness, idea or notion of resources found in **Indiana State Library**.

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Aerodynamics, Transonic
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**Aerodynamics, Transonic**represents the subject, aboutness, idea or notion of resources found in**Indiana State Library**.- Label
- Aerodynamics, Transonic

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- (EG-IN)1251833

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- XTRAN2L : a program for solving the general-frequency unsteady transonic small disturbance equation
- A computational transonic flutter boundary tracking procedure
- A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-meter transonic cryogenic tunnel
- A gridless Euler/Navier-Stokes solution algorithm for complex two-dimensional applications
- A gridless Euler/Navier-Stokes solution algorithm for complex-aircraft applications
- A linear aerodynamic analysis for unsteady transonic cascades
- A method for modifying two-dimensional adaptive wind-tunnel walls including analytical and experimental verification
- A method for the design of transonic flexible wings
- A potential-flow/boundary layer method for calculating subsonic and transonic airfoil flow with trailing-edge separation
- A review of some Reynolds number effects related to bodies at high angles of attack
- A streamwise upwind algorithm for the Euler and Navier-Stokes equations applied to transonic flows
- A study of transonic aerodynamic analysis methods for use with a hypersonic aircraft synthesis code
- A vapor generator for transonic flow visualization
- Aerodynamic design for improved maneuverability by use of three-dimensional transonic theory
- Aerodynamic design of the contoured wind-tunnel liner for the NASA supercritical, laminar-flow-control, swept-wing experiment
- An Experimental investigation of a supercritical airfoil at transonic speeds
- An analysis of three-dimensional transonic compressors
- An experimental investigation of boundary layer and crossflow characteristics of the Ames 2- by 2-foot and 11- by 11-foot transonic wind-tunnel walls
- An exploratory study of finite difference grids for transonic unsteady aerodynamics
- Analysis of the National Transonic Facility mishap
- Application of a nonisentropic full potential method to AGARD standard airfoils
- Application of the implicit MacCormack scheme to the parabolized Navier-Stokes equations
- Approximate method for calculating transonic flow about lifting wing-body configurations
- CAS22 - FORTRAN program for fast design and analysis of sock-free airfoil cascades using fictitious-gas concept
- Calculation of transonic flow in a linear cascade
- Calculation of transonic steady and oscillatory pressures on a low aspect ratio model and comparison with experiment
- Calculation of viscous effects on transonic flow for oscillating airfoils and comparisons with experiment
- Characteristic boundary conditions for three-dimensional transonic unsteady aerodynamics
- Characterization of cavity flow fields using pressure data obtained in the Langley 0.3-Meter Transonic Cryogenic Tunnel
- Comparison of calculated and measured pressures on straight-and swept-tip model rotor blades
- Comparison of calculated and measured velocities near the tip of a model rotor blade at transonic speeds
- Comparison of computational results of a few representative three-dimensional transonic potential flow analysis programs
- Comparison of the full-potential and Euler formulations for computing transonic airfoil flows
- Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds
- Computation of transonic boattail flow with separation
- Computation of unsteady transonic flows through rotating and stationary cascades
- Computational methods for unsteady transonic flows
- Computational unsteady transonic aerodynamics and aeroelasticity about airfoils and wings
- Computations for the 16-foot transonic tunnel, NASA Langley Research Center
- Computer program for calculating full potential transonic, quasi-three-dimensional flow through a rotating turbomachinery blade row
- Current status of computational methods for transonic unsteady aerodynamics and aeroelastic applications
- Designs of profiles for cascades
- Development of a multiple-parameter nonlinear perturbation procedure for transonic turbomachinery flows : preliminary application to design/optimization problems
- Development of computational methods for unsteady aerodynamics at the NASA Langley Research Center
- Effect of empennage arrangement on single engine nozzle/afterbody static pressures at transonic speeds
- Effect of nacelles on aerodynamic characteristics of an executive-jet model with simulated, partial-chord, laminar-flow-control wing glove
- Effect of non-equilibrium flow chemistry on the heating distribution over the MESUR forebody during a Martian entry
- Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads
- Effects of angle of attack and ventral fin on transonic flutter characteristics of an arrow-wing configuration
- Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds
- Entropy condtion satisfying approximations for the full potential equations of transonic flow
- Euler solutions using an implicit multigrid technique
- Evaluation of structural design concepts for an arrow-wing supersonic cruise aircraft
- Evaluation of three numerical methods for propulsion integration studies on transonic transport configurations
- Experience with transonic unsteady aerodynamic calculations
- Experimental and analytical transonic flutter characteristics of a geared-elevator configuration
- Experimental and numerical results for a generic axisymmetric single-engine afterbody with horizontal and vertical tails at transonic speeds
- Experimental cavity pressure measurements at subsonic and transonic speeds : static-pressure results
- Experimental determination of aerodynamic damping in a three-syage transonic axial-flow compressor
- Experimental study of wing leading-edge devices for improved maneuver performance of a supercritical maneuvering fighter configuration
- Experimental vibration damping characteristics of the third-stage rotor of a three-stage transonic axial-flow compressor
- Experiments and analysis concerning the use of external burning to reduce aerospace vehicle transonic drag
- F-14A aircraft high-speed flow simulations
- Feasibility of combining linear theory and impact theory methods for the analysis and design of high speed configurations
- Finite element analysis of transonic flows in cascades : importance of computational grids in improving accuracy and convergence
- Flow instabilities in transonic small disturbance theory
- Forward-swept-wing configuration designed for high maneuverability by use of a transonic computational method
- Further investigation of a finite difference procedure for analyzing the transonic flow about harmonically oscillating airfoils and wings
- Fuselage and nozzle pressure distributions of a 1/12-scale f-15 propulsion model at transonic speeds : effect of fuselage modifications and nozzle variables
- Fuselage and nozzle pressure distributions on a 1/12-scale F-15 propulsion model at transonic speeds
- High Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-meter transonic cryogenic tunnel
- High Reynolds number tests of the cast 10-2/DOA 2 airfoil in the Langley 0.3-meter transonic cryogenic tunnel - phase II
- High Reynolds number transonic tests of an NACA 0012 airfoil in the Langley 0.3-meter transonic cryogenic tunnel
- High angle canard missile test in the Ames 11-foot transonic wind tunnel
- Implicit flux-split Euler schemes for unsteady aerodynamic analysis involving unstructured dynamic meshes
- Implicit upwind-Euler solution algorithms for unstructured-grid applications
- Improved method for calculating transonic velocities on blade-to-blade stream surfaces of a turbomachine
- Improvements in the accuracy and stability of algorithms for the small-disturbance and full-potential equations applied to transonic flows
- Inlet flowfield investigation, Part I, Transonic flowfield survey
- Integration effects of pylon geometry on a high-wing transport plane
- Interactive grid generation program for CAP-TSD
- Investigation of a supersonic cruise fighter model flow field
- Investigation of the three-dimensional flow field within a transonic fan rotor : experiment and analysis
- Investigation of transonic region of high dynamic response encountered on an elastic supercritical wing
- Investigation of viscous/inviscid interaction in transonic flow over airfoils with suction
- Jet exhaust and support interference effects on the transonic aerodynamic characteristics of a fighter model with two widely spaced engines
- Laser anemometer measurements in a transonic axial-flow fan rotor
- Longitudinal aerodynamic characteristics of a generic fighter model with a wing designed for sustained transonic maneuver conditions
- Mach number effects on transonic aeroelastic forces and flutter characteristics
- Measured unsteady transonic aerodynamic characteristics of an elastic supercritical wing with an oscillating control device
- Measurements of the unsteady flow field within the stator row of a transonic axial-flow fan, II, Results and discussion
- Method to predict external store carriage characteristics at transonic speeds
- NASA supercritical airfoils : a matrix of family-related airfoils
- Navier-Stokes analysis of transonic cascade flow
- Newton like : minimal residual methods applied to transonic flow calculations
- Numerical computation of shock wave : turbulent boundary layer interaction in transonic flow over an axisymmetric curved hill
- Numerical computation of transonic flows by finite-element and finite-diffence methods
- Numerical simulation of subsonic and transonic propeller flow
- Numerical simulation of the tip vortex off a low-aspect-ratio wing at transonic speed
- Numerical solution of three-dimensional unsteady flow over wings including viscid/viscous interactions
- Numerical studies of two-dimensionsl flows
- Numerical study of porous airfoils in transonic flow
- On the instability of hypersonic flow past a wedge
- Operational manual for two-dimensional transonic code TSFOIL
- Performance characteristics of an isolated coannular plug nozzle at transonic speeds
- Perturbation solutions for transonic flow on the blade-to-blade surface of compressor blade rows
- Prediction of effects of wing contour modifications on low-speed maximum lift and transonic performance for the EA-6B aircraft
- Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel
- Pressure distributions from high Reynolds number tests of a NASA SC(3)-0712(B) airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel
- Pressure distributions from high Reynolds number transonic tests of an NACA 0012 airfoil in the Langley 0.3-meter transonic cryogenic tunnel
- Procedure for computing transonic flows for control of adaptive wind tunnels
- Progress in unstructured-grid methods development for unsteady aerodynamic applications
- Qualitative evaluation of a flush air data system at transonic speeds and high angles of attack
- Quality assessment of two- and three-dimensional unstructured meshes and validation of an upwind Euler flow solver
- Recent transonic unsteady pressure measurements at the NASA Langley Research Center
- Reduction of the shock wave intensity by modifying the transsonic blade trailing edge
- Relative efficiency and accuracy of two Navier-Stokes codes for simulating attached transonic flow over wings
- Selected topics in experimental aeroelasticity at the NASA Langley Research Center
- Separated transonic airfoil flow calculations with a nonequilibrium turbulence model
- Shock fitting applied to the prediction of high-speed rotor noise
- Simulation of transonic viscous wing and wing-fuselage flows using zonal methods
- Some anomalies observed in wind-tunnel tests of a blunt body at transonic and supersonic speeds
- Spatial adaptation procedures on tetrahedral meshes for unsteady aerodynamic flow calculations
- Spatial adaption procedures on unstructured meshes for accurate unsteady aerodynamic flow computation
- Static and dynamic pressure measurements on a NACA 0012 airfoil in the Ames High Reynolds Number Facility
- Steady and unsteady transonic small disturbance analysis of realistic aircraft configurations
- Steady- and unsteady-pressure measurements on a supercritical wing model with oscillating control surfaces at subsonic and transonic speeds
- Study of a variable sweep wing in sub or transonic flow
- Study of transonic flow over swept wings : final technical report
- Subsonic/transonic stall flutter investigation of a rotating rig
- Supercritical maneuvering fighter configuration : wind-tunnel investigation at Mach numbers of 0.60 to 0.95
- TAS--a transport aircraft/store flow field prediction code
- Test results at transonic speeds on a contoured over-the-wing propfan model
- The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil : evaluation of initial perforated configuration
- The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil : suction coefficient analysis
- The NYU inverse swept wing code
- The benchmark aeroelastic models program : description and highlights of initial results
- The design of supercritical wings by the use of three-dimensional transonic theory
- The status of analytical preparation for two-dimensional testing at high transonic speeds in the University of Southampton transonic self-streamlining wind tunnel
- Theoretical and experimental engine-inlet flow fields for fighter forebodies
- Theoretical estimation of the transonic aerodynamic characteristics of a supercritical-wing transport model with trailing-edge controls
- Theoretical/numerical study of feasibility of use of winglets on low aspect ratio wings at subsonic and transonic Mach numbers to reduce drag
- Three-dimensional flux-split Euler schemes involving unstructured dynamic meshes
- Three-dimensional transonic potential flow about complex three-dimensional configurations
- Transonic Navier-Stokes computations of strake-generated vortex interactions for a fighter-like configuration
- Transonic Navier-Stokes solutions of three-dimensional afterbody flows
- Transonic aerodynamic and aeroelastic characteristics of a variable sweep wing
- Transonic aerodynamic characteristics of a proposed assured crew return capability (ACRC) lifting-body configuration
- Transonic aerodynamics characteristics of a supercritical-wing transport model with trailing-edge controls
- Transonic aerodynamics characteristics of a supersonic cruise aircraft research model with the engines suspended above the wing
- Transonic aerodynamics of dense gases
- Transonic analysis and design of axisymmetric bodies in nonuniform flow
- Transonic and supersonic Euler computations of vortex-dominated flow fields about a generic fighter
- Transonic calculation of airfoil stability and response with active controls
- Transonic flow analysis for rotors
- Transonic flow analysis for rotors, Part 3, Three-dimensional, quasi-steady, Euler calculation
- Transonic interaction of unsteady vortical flows
- Transonic performance of a Mach 2.65 auxiliary flow axisymmetric inlet
- Transonic pressure measurements and comparison of theory to experiment for an arrow-wing configuaration
- Transonic pressure measurements and comparison of theory to experiment for three arrow-wing configurations : summary report/
- Transonic shock-induced dynamics of a flexible wing with a thick circular-arc airfoil
- Transonic unsteady aerodynamic and aeroelastic calculations about airfoils and wings
- Unsteady transonic aerodynamic and aeroelastic calculations about airfoils and wings
- Unsteady transonic algorithm improvements for realistic aircraft applications
- Unsteady transonic flow calculations for interfering lifting surface configurations
- Unsteady transonic flow calculations for realistic aircraft configurations
- Unsteady transonic flow calculations for two-dimensional canard-wing configurations with aeroelastic applications
- Unsteady transonic flow calculations for wing-fuselage configurations
- Unsteady transonic flow in cascades
- Unsteady-pressure and dynamic-deflection measurements on an aeroelastic supercritical wing
- Updated users' guide for TAWFIVE with multigrid
- Use of CYBER 203 and CYBER 205 computers for three-dimensional transonic flow calculations
- Vectorizable multigrid algorithms for transonic flow calculations
- Viscous effects on transonic airfoil stability and response
- Viscous-inviscid interaction method including wake effects for three-dimensional wing-body configurations
- Wing flutter boundary prediction using an unsteady Euler aerodynamic method

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