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f-15 aircraft

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View Development of a low-aspect ratio fin for flight research experiments By David M. Richwine

Development of a low-aspect ratio fin for flight research experiments

Development of a low-aspect ratio fin for flight research experiments

By David M. Richwine

View Flight-testing of the self-repairing flight control system using the F-15 highly integrated digital electronic control flight research facility By James F. Stewart

Flight-testing of the self-repairing flight control system using the F-15 highly integrated digital electronic control flight research facility

Flight-testing of the self-repairing flight control system using the F-15 highly integrated digital electronic control flight research facility

By James F. Stewart

View F-15B/flight test fixture II By David M. Richwine

F-15B/flight test fixture II

F-15B/flight test fixture II

By David M. Richwine

View Key topics for high-lift research By David Fisher

Key topics for high-lift research

Key topics for high-lift research

By David Fisher

View Dynamic ground-effect measurements on the F-15 STOL and Maneuver Technology Demonstrator (S/MTD) configuration By Guy T. Kemmerly

Dynamic ground-effect measurements on the F-15 STOL and Maneuver Technology Demonstrator (S/MTD) configuration

Dynamic ground-effect measurements on the F-15 STOL and Maneuver Technology Demonstrator (S/MTD) configuration

By Guy T. Kemmerly

View Application of two procedures for dual-point design of transonic airfoils By Raymond E. Mineck

Application of two procedures for dual-point design of transonic airfoils

Application of two procedures for dual-point design of transonic airfoils

By Raymond E. Mineck

View A comparison of time-optimal interception trajectories for the F-8 and F-15 By Anthony J. Calise

A comparison of time-optimal interception trajectories for the F-8 and F-15

A comparison of time-optimal interception trajectories for the F-8 and F-15

By Anthony J. Calise

View Flight characteristics of the onboard propulsion system model for the performance seeking control algorithm on an F-15 aircraft By John S. Orme

Flight characteristics of the onboard propulsion system model for the performance seeking control algorithm on an F-15 aircraft

Flight characteristics of the onboard propulsion system model for the performance seeking control algorithm on an F-15 aircraft

By John S. Orme

View A preliminary evaluation of an F100 engine parameter estimation process using flight data By Trindel A. Maine

A preliminary evaluation of an F100 engine parameter estimation process using flight data

A preliminary evaluation of an F100 engine parameter estimation process using flight data

By Trindel A. Maine

View Integrated control using the SOFFT control structure By Nesim Halyo

Integrated control using the SOFFT control structure

Integrated control using the SOFFT control structure

By Nesim Halyo

View Full flight envelope direct thrust measurement on a supersonic aircraft By Timothy R. Conners

Full flight envelope direct thrust measurement on a supersonic aircraft

Full flight envelope direct thrust measurement on a supersonic aircraft

By Timothy R. Conners

View Direct adaptive aircraft control using dynamic cell structure neural networks By Charles C. Jorgensen

Direct adaptive aircraft control using dynamic cell structure neural networks

Direct adaptive aircraft control using dynamic cell structure neural networks

By Charles C. Jorgensen

View On the use of controls for subsonic transport performance improvement By Glenn B. Gilyard

On the use of controls for subsonic transport performance improvement

On the use of controls for subsonic transport performance improvement

By Glenn B. Gilyard

View Application and flight test of linearizing transformations using measurement feedback to the nonlinear control problem By Robert F. Antoniewicz

Application and flight test of linearizing transformations using measurement feedback to the nonlinear control problem

Application and flight test of linearizing transformations using measurement feedback to the nonlinear control problem

By Robert F. Antoniewicz

View Dynamic ground effect for a cranked arrow wing airplane By Robert E. Curry

Dynamic ground effect for a cranked arrow wing airplane

Dynamic ground effect for a cranked arrow wing airplane

By Robert E. Curry

View Flight test validation of a frequency-based system identification method on an F-15 aircraft By Gerard S. Schkolnik

Flight test validation of a frequency-based system identification method on an F-15 aircraft

Flight test validation of a frequency-based system identification method on an F-15 aircraft

By Gerard S. Schkolnik

View The value of early flight evaluation of propulsion concepts using the NASA F-15 research airplane By Frank W. Burcham

The value of early flight evaluation of propulsion concepts using the NASA F-15 research airplane

The value of early flight evaluation of propulsion concepts using the NASA F-15 research airplane

By Frank W. Burcham

View Flight demonstration of a shock location sensor using constant voltage hot-film anemometry By Timothy R. Moes

Flight demonstration of a shock location sensor using constant voltage hot-film anemometry

Flight demonstration of a shock location sensor using constant voltage hot-film anemometry

By Timothy R. Moes

View Conversion from engineering units to telemetry counts on Dryden Flight simulators By Jay A. Fantini

Conversion from engineering units to telemetry counts on Dryden Flight simulators

Conversion from engineering units to telemetry counts on Dryden Flight simulators

By Jay A. Fantini

View Effect of tail size reductions on longitudinal aerodynamic characteristics of a three-surface F-15 model with nonaxisymmetric nozzles By Mark C. Frassinelli

Effect of tail size reductions on longitudinal aerodynamic characteristics of a three-surface F-15 model with nonaxisymmetric nozzles

Effect of tail size reductions on longitudinal aerodynamic characteristics of a three-surface F-15 model with nonaxisymmetric nozzles

By Mark C. Frassinelli