F-18 aircraft
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The concept F-18 aircraft represents the subject, aboutness, idea or notion of resources found in University of Missouri-St. Louis Libraries.
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F-18 aircraft
Resource Information
The concept F-18 aircraft represents the subject, aboutness, idea or notion of resources found in University of Missouri-St. Louis Libraries.
- Label
- F-18 aircraft
- Source
- nasat
46 Items that share the Concept F-18 aircraft
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- Water-tunnel study results of a TF/A-18 and F/A-18 canopy flow visualization
- A method for integrating thrust-vectoring and actuated forebody strakes with conventional aerodynamic controls on a high-performance fighter airplane
- A simple dynamic engine model for use in a real-time aircraft simulation with thrust vectoring
- Active aeroelastic wing aerodynamic model development and validation for a modified F/A-18A airplane
- Advances in experiment design for high performance aircraft : paper no. 8
- Aeroservoelastic modeling and validation of a thrust-vectoring F/A-18 aircraft
- An evaluation technique for an F/A-18 aircraft loads model using F/A-18 systems research aircraft flight data
- An inlet distortion assessment during aircraft departures at high angle of attack for an F/A-18A aircraft
- An overview of the NASA F-18 High Alpha Research Vehicle
- CFL3D, its history and some recent applications
- Design and development of an F/A-18 inlet distortion rake : a cost and time saving solution
- Design and integration of an actuated nose strake control system
- Design and integration of an actuated nose strake control system
- Design of low complexity model reference adaptive controllers
- Development and testing of control laws for the active aeroelastic wing program
- 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
- Estimating engine airflow in gas-turbine powered aircraft with clean and distorted inlet flows
- Evaluation of gritting strategies for high angle of attack using wind tunnel and flight test data for the F/A-18
- Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack
- Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack
- F-18 High Alpha Research Vehicle surface pressures : initial in-flight results and correlation with flow visualization and wind-tunnel data
- F/A-18A inlet flow characteristics during maneuvers with rapidly changing angle of attack
- Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft
- Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft
- Fiber optic experience with the smart actuation system on the F-18 systems research aircraft
- Flight testing of the space launch system (SLS) adaptive augmenting control (AAC) algorithm on an F/A-18
- 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
- Flutter clearance of the F-18 high-angle-of-attack research vehicle with experimental wingtip instrumentation pods
- Forebody flow visualization on the F-18 HARV with actuated forebody strakes
- High-Alpha handling qualities flight research on the NASA F/A-18 High Alpha Research Vehicle
- High-alpha research vehicle lateral-directional control law description, analyses, and simulation results
- Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60 ° angle of attack
- Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60 ̊angle of attack : contract NAS 3-26617
- Loads model development and analysis for the F/A-18 Active Aeroelastic Wing airplane
- Modeling of aircraft unsteady aerodynamic characteristics, Part 3, Parameters estimated from flight data
- Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0 t̊o 70
- Nonclassical flight control for unhealthy aircraft : final report : (March 28, 1997-November 30, 1997)
- Overview of HATP experimental aerodynamics data for the baseline F/A-18 configuration : High-Angle-of-Attack Technology Conference
- Performance of an electro-hydrostatic actuator on the F-18 systems research aircraft
- Preliminary results from an airdata enhancement algorithm with application to high-angle-of-attack flights
- Production support flight control computers : research capability for F/A-18 aircraft at Dryden Flight Research Center
- Spatial characteristics of the unsteady differential pressures on 16% F/A-18 vertical tails : 36th Aerospace Sciences meeting & exhibit : January 12-15, 1998/Reno, NV
- Summary of in-flight flow visualization obtained from the NASA high alpha research vehicle
- Thrust vectoring on the NASA F-18 high alpha research vehicle
- Thrust vectoring on the NASA F-18 high alpha research vehicle
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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/tyzOCB3Aakc/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.umsl.edu/resource/tyzOCB3Aakc/">F-18 aircraft</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>
