NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Fourth High Alpha Conference, volume 1The goal of the Fourth High Alpha Conference, held at the NASA Dryden Flight Research Center on July 12-14, 1994, was to focus on the flight validation of high angle-of-attack technologies and provide an in-depth review of the latest high angle-of-attack activities. Areas that were covered include, high angle-of-attack aerodynamics, propulsion and inlet dynamics, thrust vectoring, control laws and handling qualities, tactical utility, and forebody controls.
Document ID
19950007815
Acquisition Source
Armstrong Flight Research Center
Document Type
Conference Publication (CP)
Date Acquired
September 6, 2013
Publication Date
July 1, 1994
Publication Information
Publisher: National Aeronautics and Space Administration
Volume: 1
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.55:10143-VOL-1
H-2007-VOL-1
NASA-CP-10143-VOL-1
Report Number: NAS 1.55:10143-VOL-1
Report Number: H-2007-VOL-1
Report Number: NASA-CP-10143-VOL-1
Meeting Information
Meeting: 4th High Alpha Conference
Location: Edwards, CA
Country: US
Start Date: July 12, 1994
End Date: July 14, 1994
Sponsors: National Aeronautics and Space Administration
Accession Number
95N14229
Funding Number(s)
PROJECT: RTOP 505-68-30
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Keywords
Aerodynamics
F-18 HARV
High angle of attack
X-31 aircraft

Related Records

IDRelationTitle19950007816WorkHigh Alpha Technology Program (HATP) ground test to flight comparisons19950007821WorkParameter identification for X-31A at high angles of attack19950007817WorkFlight and full-scale wind-tunnel comparison of pressure distributions from an F-18 aircraft at high angles of attack19950007822WorkValidation of the NASA Dryden X-31 simulation and evaluation of mechanization techniques19950007819WorkHybrid structured/unstructured grid computations for the F/A-18 at high angle of attack19950007818WorkNumerical simulation of the flow about an F-18 aircraft in the high-alpha regime19950007823WorkFree-to-roll tests of X-31 and F-18 subscale models with correlation to flight test results19950007820WorkComparison of X-31 flight, wind-tunnel, and water-tunnel yawing moment asymmetries at high angles of attack19950007824See AlsoStatic and dynamic force/moment measurements in the Eidetics water tunnel19950007826WorkF-18 high alpha research vehicle: Lessons learned19950007827WorkDesign and development of an F/A-18 inlet distortion rake: A cost and time saving solution19950007828WorkX-31 post-stall envelope expansion and tactical utility testing19950007829WorkX-31 quasi-tailless flight demonstration19950007830WorkX-31 high angle of attack control system performance19950007831WorkFlight test results of the F-16 aircraft modified with the axisymmetric vectoring exhaust nozzle19950007832WorkFlight validation of ground-based assessment for control power requirements at high angles of attack19950007833WorkHigh angle of attack flying qualities criteria for longitudinal rate command systems19950007834WorkVista/F-16 Multi-Axis Thrust Vectoring (MATV) control law design and evaluation19950007835WorkMulti-application controls: Robust nonlinear multivariable aerospace controls applications19950007836WorkCombat Agility Management System (CAMS)19950007826WorkF-18 high alpha research vehicle: Lessons learned19950007827WorkDesign and development of an F/A-18 inlet distortion rake: A cost and time saving solution19950007828WorkX-31 post-stall envelope expansion and tactical utility testing19950007829WorkX-31 quasi-tailless flight demonstration19950007830WorkX-31 high angle of attack control system performance19950007831WorkFlight test results of the F-16 aircraft modified with the axisymmetric vectoring exhaust nozzle19950007832WorkFlight validation of ground-based assessment for control power requirements at high angles of attack19950007833WorkHigh angle of attack flying qualities criteria for longitudinal rate command systems19950007834WorkVista/F-16 Multi-Axis Thrust Vectoring (MATV) control law design and evaluation19950007835WorkMulti-application controls: Robust nonlinear multivariable aerospace controls applications19950007836WorkCombat Agility Management System (CAMS)
No Preview Available