Hugh L. Dryden Flight Research Center
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The organization Hugh L. Dryden Flight Research Center represents an institution, an association, or corporate body that is associated with resources found in Indiana State Library.
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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 Indiana State Library.
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- Hugh L. Dryden Flight Research Center
- Authority link
- (EG-IN)1068833
71 Items by the Organization Hugh L. Dryden Flight Research Center
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- 1996 NASA-ASEE-Stanford Summer Faculty Fellowship Program : administrative & summary technical reports : NASA Ames Research Center, grant no. NGT 2-52212
- A characterization of the real zeros of a particular transcendental function
- 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
- AFTI/F-111 MAW flight control system and redundancy management description
- Aerodynamic characteristics of a vane flow angularity sensor system capable of measuring flightpath accelerations for the mach number range from 0.40 to 2.54
- Aerodynamic derivatives for an oblique wing aircraft estimated from flight data by using a maximum likelihood technique
- Aircraft ground vibration testing at the NASA Dryden Flight Research Facility, 1993
- Airdata measurement and calibration
- An efficient code for the simulation of nonhydrostatic stratified flow over obstacles
- Anomalous buckling characteristics of laminated metal-matrix composite plates with central square holes
- Application of a performance modeling technique to an airplane with variable sweep wings
- Automated testing experience of the linear aerospike SR-71 experiment (LASRE) controller
- 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
- Comparison of calculated and altitude-facility-measured thrust and airflow of two prototype F100 turbofan engines
- Comparison of concurrent strain gage- and pressure transducer-measured flight loads on a lifting reentry vehicle and correlation with wind tunnel predictions
- Comparison of three thrust calculation methods using in-flight thrust data
- Conversion from engineering units to telemetry counts on Dryden Flight simulators
- Design and evaluation of a new boundary-layer rake for flight testing
- Determination of sun angles for observations of shock waves on a transport aircraft / : David F. Fisher ... [and others]
- Development and flight test results of an autothrottle control system at Mach 3 cruise
- Diversity techniques for omnidirectional telemetry coverage of the HiMAT research vehicle
- Effect of an alternate winglet on the pressure and spanwise load distributions of a first-generation jet transport wing
- Effect of number of probes and their orientation on the calculation of several compressor face distortion descriptors
- Effects of fuselage forebody geometry on low-speed lateral-directional characteristics of twin-tail fighter model at high angles of attack
- Elastic constants for superplastically formed/diffusion bonded corrugated sandwich core
- Estimated benefits of variable-geometry wing camber control for transport aircraft
- Evaluation of a simplified gross thrust calculation technique using two prototype F100 turbofan engines in an altitude facility
- Evaluation of an envelope-limiting device using simulation and flight test of a remotely piloted research vehicle
- Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft
- Flight comparison of the transonic agility of the F-111A airplane and the F-111 supercritical wing airplane
- Flight evaluation of a simplified gross thrust calculation technique using an F100 turbofan engine in an F-15 airplane
- Flight-determined stability and control derivatives for the F-111 TACT research 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
- Flight-measured afterbody pressure coefficients from an airplane having twin side-by-side jet engines for Mach numbers from 0.6 to 1.6
- 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
- Ground-recorded sonic boom signatures of F-18 aircraft in formation flight
- High-angle-of-attack yawing movement asymmetry of the X-31 aircraft from flight test
- Historical background and design evolution of the transonic aircraft technology supercritical wing
- Important factors in the maximum likelihood analysis of flight test maneuvers
- Improved test methods for determining lightning-induced voltages in aircraft
- In-flight boundary-layer measurements on a hollow cylinder at a Mach number of 3.0
- In-flight demonstration of a Real-Time Flush Airdata Sensing (RT-FADS) system
- Initial flight test of the production support flight control computers at NASA Dryden Flight Research Center
- Landing approach airframe noise measurement and analysis
- Limited evaluation of an F-14A airplane utilizing an aileron-rudder inter-connect control system in the landing configuration
- Measurements and predictions of flyover and static noise of a TF30 afterburning turbofan engine
- Pegasus wing-glove experiment to document hypersonic crossflow transition : measurement system and selected flight results
- Performance evaluation method for dissimilar aircraft designs
- Performance of an electro-hydrostatic actuator on the F-18 systems research aircraft
- Practical aspects of using a maximum likelihood estimation method to extract stability and control derivitives from flight data
- Precision controllability of the F-15 airplane
- Precision controllability of the FY-17 airplane
- Programmer's manual for MMLE3, a general FORTRAN program for maximum likelihood parameter estimation
- Real-time method for estimating viscous forebody drag coefficients
- 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
- Reynolds number effects at high angles of attack
- Similitude requirements and scaling relationships as applied to model testing
- Simulator evaluation of simplified propulsion-only emergency flight control systems on transport aircraft
- Stability and control of the Gossamer human-powered aircraft by analysis and flight test
- Subsonic tests of an all-flush-pressure-orifice air data system
- The X-33 extended flight test range
- The theory and practice of estimating the accuracy of dynamic flight-determined coefficients
- The use of a lidar forward-looking turbulence sensor for mixed-compression inlet unstart avoidance and gross weight reduction on a high speed civil transport
- Thermal modeling and analysis of a cryogenic tank design exposed to extreme heating profiles
- Unsteady aerodynamics : subsonic compressible inviscid case
- User's manual for MMLE3, a general FORTRAN program for maximum likelihood parameter estimation
- Web-based instruction and learning : analysis and needs assessment
- Wind tunnel investigation of an all flush orifice air data system for a large subsonic aircraft
- Wind-tunnel investigations of blunt-body drug reduction using forebody surface roughness
- X-1 paper glider kit : investigating the basics of flight with a model of the first supersonic aircraft
- X-Gliders : exploring flight research with experimental gliders
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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.library.in.gov/resource/FjGlsrHEz6Y/" typeof="Organization http://bibfra.me/vocab/lite/Organization"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.library.in.gov/resource/FjGlsrHEz6Y/">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.library.in.gov/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.library.in.gov/">Indiana State Library</a></span></span></span></span></div>
