Hugh L. Dryden Flight Research Center
Resource Information
The organization Hugh L. Dryden Flight Research Center represents an institution, an association, or corporate body that is associated with resources found in University of Missouri-St. Louis Libraries.
The Resource
Hugh L. Dryden Flight Research Center
Resource Information
The organization Hugh L. Dryden Flight Research Center represents an institution, an association, or corporate body that is associated with resources found in University of Missouri-St. Louis Libraries.
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- Hugh L. Dryden Flight Research Center
93 Items by the Organization Hugh L. Dryden Flight Research Center
1 Items that are about the Organization Hugh L. Dryden Flight Research Center
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Context of Hugh L. Dryden Flight Research CenterContributor of
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- X-Gliders : exploring flight research with experimental gliders
- 1996 NASA-ASEE-Stanford Summer Faculty Fellowship Program : administrative & summary technical reports : NASA Ames Research Center, grant no. NGT 2-52212
- A base drag reduction experiment on the X-33 Linear Aerospike SR-71 Experiment (LASRE) flight program
- A conversion of wheatstone bridge to current-loop signal conditioning for strain gages
- A modified T-value method for selection of strain gages for measuring loads on a low aspect ratio wing
- A parallel, finite-volume algorithm for large-eddy simulation of turbulent flows
- AMT-200S motor glider parameter and performance estimation
- Active aeroelastic wing aerodynamic model development and validation for a modified F/A-18A airplane
- Aircraft ground vibration testing at the NASA Dryden Flight Research Facility, 1993
- In-flight boundary-layer measurements on a hollow cylinder at a Mach number of 3.0
- In-flight boundary-layer transition on a large flat plate at supersonic speeds
- In-flight demonstration of a Real-Time Flush Airdata Sensing (RT-FADS) system
- Loads model development and analysis for the F/A-18 Active Aeroelastic Wing airplane
- Local flow conditions for proplusion experiments on the F-15B Propulsion Flight Test Fixture
- Methods for in-flight wing shape predictions of highly flexible unmanned aerial vehicles : formulation of Ko displacement theory
- Mission information and test systems summary of accomplishments, 2011
- Modal filtering for control of flexible aircraft
- NASA Global Hawk : a new tool for Earth science research
- Optimal pitch thrust-vector angle and benefits for all flight regimes
- Orion Pad Abort 1 Crew Module mass properties test approach and results
- Pegasus wing-glove experiment to document hypersonic crossflow transition : measurement systems and selected flight results
- Performance of an electro-hydrostatic actuator on the F-18 systems research aircraft
- Proposed flight research of a dual-bell rocket nozzle using the NASA F-15 airplane
- Recent flight test results of the joint CIAM-NASA Mach 6.5 Scramjet Flight Program
- Reconfigurable flight control designs with application to the X-33 vehicle
- Reduced uncertainties in the flutter analysis of the aerostructures test wing
- Reynolds number effects at high angles of attack
- Sensor-only system identification for structural health monitoring of advanced aircraft
- Survey of applications of active control technology for gust alleviation and new challenges for lighter-weight aircraft
- Tailored excitation for frequency response measurement applied to the X-43A flight vehicle
- The X-33 extended flight test range
- Thermal modeling and analysis of a cryogenic tank design exposed to extreme heating profiles
- Thermostructural analysis of the SOFIA fine field and wide field imagers subjected to convective thermal shock
- Thermostructural behavior of a hypersonic aircraft sandwich panel subjected to heating on one side
- Thrust vectoring on the NASA F-18 high alpha research vehicle
- Titanium honeycomb panel testing
- Unsteady aerodynamic model tuning for precise flutter prediction
- Unsteady aerodynamics : subsonic compressible inviscid case
- User's manual for MMLE3, a general FORTRAN program for maximum likelihood parameter estimation
- Virtual deformation control of the X-56A model with simulated fiber optic sensors
- Web-based instruction and learning : analysis and needs assessment
- Wind-tunnel and flight-test results for the measurements of flow variables at supersonic speeds using improved wedge and conical probes
- Wind-tunnel investigations of blunt-body drag reduction using forebody surface roughness
- X-1 paper glider kit : investigating the basics of flight with a model of the first supersonic aircraft
- Airdata measurement and calibration
- An impact-location estimation algorithm for subsonic uninhabited aircraft
- An indirect system identification technique for stable estimation of continuous-time parameters of the vestibulo-ocular reflex (VOR)
- An overview of NASA's Subsonic Research Aircraft Testbed (SCRAT)
- Analysis of low-speed stall aerodynamics of a swept wing with laminar-flow glove
- Anomalous buckling characteristics of laminated metal-matrix composite plates with central square holes
- Application of approximate unsteady aerodynamics for flutter analysis
- Applications of Ko displacement theory to the deformed shape predictions of the doubly-tapered Ikhana wing
- Automated testing experience of the Linear Aerospike SR-71 Experiment (LASRE) controller
- Basis function approximation of transonic aerodynamic influence coefficient matrix
- Boundary-layer transition results from the F-16XL-2 supersonic laminar flow control experiment
- Centennial of flight, 1903-2003
- Comparative optical measurements of airspeed and aerosols on a DC-8 aircraft
- Complexity and pilot workload metrics for the evaluation of adaptive flight controls on a full scale piloted aircraft
- Conversion from engineering units to telemetry counts on Dryden Flight simulators
- Data driven model development for the supersonic semispan transport (S4T)
- Deformed shape calculation of a full-scale wing using fiber optic strain data from a ground loads test
- Design and calibration of an airborne multichannel swept-tuned spectrum analyzer
- Design and evaluation of a new boundary layer rake for flight testing
- Design and flight evaluation of a new force-based angle probe
- Design of low complexity model reference adaptive controllers
- Determination of sun angles for observations of shock waves on a transport aircraft : David F. Fisher ... [et al.]
- Development and flight test of an emergency flight control system using only engine thrust on an MD-11 transport airplane
- Development and testing of control laws for the active aeroelastic wing program
- Development of a closed-loop strap down attitude system for an ultrahigh altitude flight experiment
- Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV
- Effects of inlet distortion on a static pressure probe mounted on the engine hub in an F-15 airplane
- Estimation of modal parameters using a wavelet-based approach
- Experimental and numerical characterization of a steady-state cylindrical blackbody cavity at 1100 degrees celsius
- Extension of Ko straight-beam displacement theory to deformed shape predictions of slender curved structures
- First- and second-order displacement transfer functions for structural shape calculations using analytically predicted surface strains
- Flight evaluation of a simplified gross thrust calculation technique using an F100 turbofan engine in an F-15 airplane
- Flight evaluation of an aircraft with side and center stick controllers and rate-limited ailerons
- Flight test of a propulsion-based emergency control system on the MD-11 airplane with emphasis on the lateral axis
- Flight test of an adaptive configuration optimization system for transport aircraft
- Flight test results from the rake airflow gage experiment on the F-15B airplane
- Flight test results on the stability and control of the F-15 Quiet Spike aircraft
- Flight-determined, subsonic, lateral-directional stability and control derivatives of the thrust-vectoring F-18 high angle of attack research vehicle (HARV), and comparisons to the basic F-18 and predicted derivates
- Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model
- Forebody flow visualization on the F-18 HARV with actuated forebody strakes
- Frequency shift during mass properties testing using compound pendulum method
- Further development of Ko displacement theory for deformed shape predictions of nonuniform aerospace structures
- Ground-recorded sonic boom signatures of F-18 aircraft in formation flight
- High-Alpha handling qualities flight research on the NASA F/A-18 High Alpha Research Vehicle
- High-angle-of-attack yawing movement asymmetry of the X-31 aircraft from flight test
- High-temperature modal survey of a hot-structure control surface
- Important factors in the maximum likelihood analysis of flight test maneuvers
- Improved displacement transfer functions for structure deformed shape predictions using discretely distributed surface strains
- Improved test methods for determining lightning-induced voltages in aircraft
Focus of
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- Airdata measurement and calibration
- A base drag reduction experiment on the X-33 Linear Aerospike SR-71 Experiment (LASRE) flight program
- Mission information and test systems summary of accomplishments, 2011
- An indirect system identification technique for stable estimation of continuous-time parameters of the vestibulo-ocular reflex (VOR)
- Modal filtering for control of flexible aircraft
- Estimation of modal parameters using a wavelet-based approach
- An overview of NASA's Subsonic Research Aircraft Testbed (SCRAT)
- Wind-tunnel investigations of blunt-body drag reduction using forebody surface roughness
- Analysis of low-speed stall aerodynamics of a swept wing with laminar-flow glove
- Reconfigurable flight control designs with application to the X-33 vehicle
- Experimental and numerical characterization of a steady-state cylindrical blackbody cavity at 1100 degrees celsius
- Wind-tunnel and flight-test results for the measurements of flow variables at supersonic speeds using improved wedge and conical probes
- Automated testing experience of the Linear Aerospike SR-71 Experiment (LASRE) controller
- Optimal pitch thrust-vector angle and benefits for all flight regimes
- First- and second-order displacement transfer functions for structural shape calculations using analytically predicted surface strains
- Improved displacement transfer functions for structure deformed shape predictions using discretely distributed surface strains
- A modified T-value method for selection of strain gages for measuring loads on a low aspect ratio wing
- Flight evaluation of an aircraft with side and center stick controllers and rate-limited ailerons
- A parallel, finite-volume algorithm for large-eddy simulation of turbulent flows
- Virtual deformation control of the X-56A model with simulated fiber optic sensors
- Orion Pad Abort 1 Crew Module mass properties test approach and results
- Flight test of an adaptive configuration optimization system for transport aircraft
- Deformed shape calculation of a full-scale wing using fiber optic strain data from a ground loads test
- Thermostructural analysis of the SOFIA fine field and wide field imagers subjected to convective thermal shock
- Flight test results on the stability and control of the F-15 Quiet Spike aircraft
- Design and calibration of an airborne multichannel swept-tuned spectrum analyzer
- Design and evaluation of a new boundary layer rake for flight testing
- In-flight boundary-layer transition on a large flat plate at supersonic speeds
- Pegasus wing-glove experiment to document hypersonic crossflow transition : measurement systems and selected flight results
- Sensor-only system identification for structural health monitoring of advanced aircraft
- Design of low complexity model reference adaptive controllers
- Proposed flight research of a dual-bell rocket nozzle using the NASA F-15 airplane
- Survey of applications of active control technology for gust alleviation and new challenges for lighter-weight aircraft
- Development and flight test of an emergency flight control system using only engine thrust on an MD-11 transport airplane
- Frequency shift during mass properties testing using compound pendulum method
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<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.umsl.edu/resource/EuysRIOeimA/" typeof="Organization http://bibfra.me/vocab/lite/Organization"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.umsl.edu/resource/EuysRIOeimA/">Hugh L. Dryden Flight Research Center</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.umsl.edu/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.umsl.edu/">University of Missouri-St. Louis Libraries</a></span></span></span></span></div>
