#
Aerodynamics
Resource Information
The concept ** Aerodynamics** represents the subject, aboutness, idea or notion of resources found in **Houston Public Library**.

The Resource
Aerodynamics
Resource Information

The concept

**Aerodynamics**represents the subject, aboutness, idea or notion of resources found in**Houston Public Library**.- Label
- Aerodynamics

- Source
- nasat

## Context

Context of Aerodynamics#### Subject of

- A CFD/CSD interaction methodology for aircraft wings : a dissertation ...
- A Laser velocimeter system for large-scale aerodynamic testing
- A PDE sensitivity equation method for optimal aerodynamic design
- A correlation between flight-determined derivatives and wind-tunnel data for the X-24B research aircraft
- A parametric study of accelerations of an airplane due to a wake vortex system
- A parametric study of accelerations of an airplane due to a wake vortex system
- A preliminary look at techniques used to obtain airdata from flight at high angles of attack
- A review of 50 years of aerodynamic research with NACA/NASA
- A scalable parallel cell-projection volume rendering algorithm for three-dimensional unstructured data
- A survey of challenges in aerodynamic exhaust nozzle technology for aerospace propulsion applications
- A survey of challenges in aerodynamic exhaust nozzle technology for aerospace propulsion applications
- A tomographic technique for aerodynamics at transonic speeds
- A user's guide to CGNS
- A workshop based simulator for teaching compressible aerodynamics
- AMT-200S motor glider parameter and performance estimation
- Aerodynamic design of a propeller for high-altitude balloon trajectory control
- Aerodynamic design on unstructured grids for turbulent flows
- Aerodynamic design optimization on unstructured grids with a continuous adjoint formulation
- Aerodynamic design optimization via reduced Hessian SQP with solution refining
- Aerodynamic design optimization with sensitivity analysis and computational fluid dynamics
- Aerodynamic evaluation of two compact radial inflow turbine rotors
- Aerodynamic parameter estimation via fourier modulating function techniques
- Aerodynamics and heat transfer investigations on a high Reynolds number turbine cascade
- Aerodynamics of 3-dimensional bodies in transitional flow
- Aerodynamics of a transitioning turbine stator over a range of Reynolds numbers
- Aerodynamics of a transitioning turbine stator over a range of Reynolds numbers
- Aeroelastic analysis of aircraft : wing and wing/fuselage configurations
- Airframe technology for aircraft energy efficiency
- An evaluation of an analytical simulation of an airplane with tailplane icing by comparision to flight data
- An experimental evaluation of the performance of two combination pitot pressure probes
- An experimental study of the aerodynamics of a NACA0012 airfoil with a simulated glaze ice accretion, Volume II
- An interactive software for conceptual wing flutter analysis and parametric study
- An interactive software for conceptual wing flutter analysis and parametric study
- An overview of aerodynamic research and technology requirements as related to some military needs
- An overview of the NASA F-18 high alpha research vehicle
- An overview of three approaches to multidisciplinary aeropropulsion simulations
- An overview of three approaches to multidisciplinary aeropropulsion simulations
- Analysis of small-scale rotor hover performance data
- Application of a linearized unsteady aerodynamic analysis to standard cascade configurations
- Application of approximate unsteady aerodynamics for flutter analysis
- Assessment of aerodynamic challenges of a variable-speed power turbine for large civil tilt-rotor application
- Astrop3 user's guide
- Autonomous momentum management for space station : final report, 15 October 1984
- CFD analysis and design optimization using parallel computers
- CFL3D, its history and some recent applications
- Computational aerodynamics and supercomputers
- Computational fluid dynamics (CFD) simulation of hypersonic turbine-based combined-cycle (TBCC) inlet mode transition
- Computational fluid dynamics at NASA Ames and the numerical aerodynamic simulation program
- Computational fluid dynamics uses in fluid dynamics/aerodynamics education
- Computer simulation of aircraft aerodynamics
- Continued development and application of circulation control pneumatic technology to advanced transport aircraft : NASA grant NAG-1-1517 : period covered, June 14, 1993 to August 31, 1997
- Control activity in support of NASA Turbine Based Combined Cycle (TBCC) research
- Coordinates for a high performance 4:1 pressure ratio centrifugal compressor
- Data mining of NASA Boeing 737 flight data : frequency analysis of in-flight recorded data
- Design guide for aerodynamics testing of Earth and planetary entry vehicles in a ballistic range
- Design of a slotted, natural-laminar-flow airfoil for business-jet applications
- Design-of-experiments to reduce life-cycle costs in combat aircraft inlets
- Design-of-experiments to reduce life-cycle costs in combat aircraft inlets
- Development of a new instrument for direct skin friction measurements : final report for NASA grant NAG 1-303
- Development of an open rotor cycle model in NPSS using a multi-design point approach
- Development of direct-inverse 3-D method for applied aerodynamic design and analysis : semiannual progress report, July 1, 1986 - December 31, 1986
- Development of experimental icing simulation capability for full-scale swept wings : hybrid design process, years 1 and 2
- Development of multiobjective optimization techniques for sonic boom minimization
- Development of the Transport Class Model (TCM) aircraft simulation from a sub-scale Generic Transport Model (GTM) simulation
- Development, analysis and testing of the High Speed Research Flexible Semispan Model
- Direct harmonic linear Navier-Stokes methods for efficient simulation of wave packets
- Dynamic analysis of rotor blade undergoing rotor power shutdown
- Dynamic ground effect for a cranked arrow wing airplane
- Dynamic modeling of starting aerodynamics and stage matching in an axi-centrifugal compressor
- Dynamic modeling of starting aerodynamics and stage matching in an axi-centrifugal compressor
- Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV
- Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV
- Effect of control surface mass unbalance on the stability of a closed-loop active control system
- Enhancement/upgrade of Engine Structures Technology Best Estimator (EST/BEST) software system
- Enhancing the remote variable operations in NPSS/CCDK
- Essential elements of computational algorithms for aerodynamic analysis and design : under contracts NAS1-97046 & NAS1-19480
- Experimental performance and analysis of 15.04-centimeter-tip-diameter, radial-inflow turbine with work factor of 1.126 and thick blading
- F-18 high research vehicle (HARV) parameter identification flight test maneuvers for optimal input design validation and lateral control effectiveness
- Finite element modeling and analysis of Mars entry aeroshell concept
- Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements
- Flight Mechanics/Estimation Theory Symposium, 1990 : proceedings of a symposium sponsored by NASA Goddard Space Flight Center and held at Goddard Space Flight Center, Greenbelt, Maryland, May 22-24, 1990
- Flight research at Ames : fifty-seven years of development and validation of aeronautical technology
- Flight test identification and simulation of a UH-60A helicopter and slung load
- Fourth High Alpha Conference, NASA Dryden Flight Research Center, Edwards, California, July 12-14, 1994
- Full-potential modeling of blade-vortex interactions
- Further evaluation of scaling methods for rotorcraft icing
- Guide to AERO2S and WINGDES computer codes for prediction and minimization of drag due to lift
- HBCUs Research Conference agenda and abstracts : proceedings of a conference held at and sponsored by Ohio Aerospace Institute, Cleveland, Ohio, April 8-9, 1998
- Hi-alpha forebody design
- High Reynolds number hybrid laminar flow control (HLFC) flight experiment, II, Aerodynamic design
- High fidelity CFD analysis and validation of rotorcraft gearbox aerodynamics under operational and oil-out conditions : final report
- High speed civil transport
- Ice accretions and full-scale iced aerodynamic performance data for a two-dimensional NACA 23012 airfoil
- Icing simulation : a survey of computer models and experimental facilities
- In-flight aerodynamic measurements of an iced horizontal tailplane
- Integration of a CAD system into an MDO framework
- Interactive computer graphics applications for compressible aerodynamics
- Introduction of the ASP3D computer program for unsteady aerodynamic and aeroelastic analyses
- Introductions to generalized functions with applications in aerodynamics and aeroacoustics
- Inverse design technique for cascades
- Investigation of chemically-reacting supersonic internal flows
- Joint University Program for Air Transportation Research-1986 : proceedings of a conference
- Key topics for high-lift research : a joint wind tunnel/flight test approach : report for NASA-Ames University consortium, joint research interchange, May 1, 1995 - September 30, 1996
- Kinematics, influence functions and field quantities for disturbance propagation from moving disturbance sources
- Laser pencil beam based techniques for visualization and analysis of interfaces between media
- Laser scanning system for pressure and temperature paints : final report, NASA NCC2-5115
- Mach 10 computational study of a three-dimensional scramjet inlet flow field
- Missile aerodynamics for ascent and re-entry
- Modeling of vortex-induced oscillations based on indicial response approach
- Multi-objective optimization of a turbofan for an advanced, single-aisle transport
- Multidisciplinary design optimization using multiobjective formulation techniques : final report on NASA Ames grant no. NCA2-778
- Nonlinear aerodynamic modeling from flight data using advanced piloted maneuvers and fuzzy logic
- Numerical approach for the aerodynamic analysis of airfoils with laminar separation
- Numerical study of boundary-layer control in aerodynamics : final technical report for grant NCC 2-845, NASA-Ames Research Center; grant period: 1 January 1994 to 31 December 1995, no-cost extension to 31 December 1996
- Numerical study of three-dimensional separation and flow control at a wing-body junction : progress report for the period ended April 30, 1989
- Optimal regulation in systems with stochastic time sampling
- Optimum aerodynamic design via boundary control
- Overview of HATP experimental aerodynamics data for the baseline F/A-18 configuration : High-Angle-of-Attack Technology Conference
- PLTTER user's guide
- PLTTER user's guide
- PROFILE : airfoil geometry manipulation and display : user's guide
- Parallel visualization of large-scale aerodynamics calculations : a case study on the Cray T3E
- Parallelization of a parabolized Navier-Stokes solver with a design optimizer : 34th AIAA Aerospace Sciences Meeting and Exhibit
- Potential impacts of advanced aerodynamic technology on air transportation system productivity
- Prediction of complex aerodynamic flows with explicit algebraic stress models : 34th Aerospace Sciences Meeting & Exhibit, January 15-18, 1996/Reno, NV
- Prediction of forces and moments for flight vehicle control effectors
- Preliminary sizing of vertical take-off rocket-based combined-cycle powered launch vehicles
- Preliminary sizing of vertical take-off rocket-based combined-cycle powered launch vehicles
- Remote sensing/global change : a special bibliography
- Research opportunities in advanced aerospace concepts
- Research opportunities in advanced aerospace concepts
- Review of research on angle-of-attack indicator effectiveness
- Rotary-wing relevant compressor aero research and technology development activities at Glenn Research Center
- Rotating rig development for droplet deformation/breakup and impact induced by aerodynamic surfaces
- SR-SCARLET 1 : Peregrin
- STARS, an integrated, multidisciplinary, finite-element, structural, fluids, aeroelastic, and aeroservoelastic analysis computer program
- Sensor-only system identification for structural health monitoring of advanced aircraft
- Simulation of iced wing aerodynamics
- Some thoughts concerning large load-carrying vehicles
- Study of potential aerodynamic benefits from spanwise blowing at wingtip
- Subsonic dynamics of stardust sample return capsule
- Subsonic dynamics of stardust sample return capsule
- Swept-wing ice accretion characterization and aerodynamics
- Tabulation of data from the tip aerodynamics and acoustics test
- Technology benefits and ground test facilities for high-speed civil transport development
- Test devices for aeronautical research and technology
- Testing, analysis, and code verification of aerodynamics and heat transfer related to turbomachinery : final report
- The aluminum falcon : a low cost modern commercial transport
- The effects of Reynolds number, motor incidence angle and surface roughness on the heat transfer distribution in a large-scale turbine rotor passage
- The effects of Reynolds number, rotor incidence angle and surface roughness on the heat transfer distribution in a large-scale turbine rotor passage
- The effects of inlet turbulence and rotor/stator interactions on the aerodynamics and heat transfer of a large-scale rotating turbine model : IV--aerodynamic data tabulation
- Transonic dynamics tunnel force and pressure data acquired on the HSR rigid semispan model
- Turbulence intensity at inlet of 80- by 120-foot wind tunnel caused by upwind blockage
- Unsteady aero computation of a 1 1/2 stage large scale rotating turbine
- Unsteady three-dimensional flow separation
- VORCOR : a computer program for calculating characteristics of wings with edge vortex separation by using a vortex filament and core model
- Validation of design and analysis techniques of tailored composite structures
- Variable-speed power-turbine for the large civil tilt rotor
- Variable-speed power-turbine research at Glenn Research Center
- Water-tunnel study results of a TF/A-18 and F/A-18 canopy flow visualization
- X based interactive computer graphics applications for aerodynamic design and education
- [Research in progress in applied mathematics, numerical analysis, fluid mechanics, and computer science : semiannual report, October 1, 1993 through March 31, 1994

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