Nothing Special   »   [go: up one dir, main page]

Orme et al., 1999 - Google Patents

Selected performance measurements of the F-15 ACTIVE axisymmetric thrust-vectoring nozzle

Orme et al., 1999

View PDF
Document ID
6094374189113813792
Author
Orme J
Sims R
Publication year

External Links

Snippet

Flight tests recently completed at the NASA Dryden Flight Research Center evaluated performance of a hydromechanically vectored axisymmetric nozzle onboard the F-15 ACTIVE. A flight-test technique whereby strain gages installed onto engine mounts provided …
Continue reading at ntrs.nasa.gov (PDF) (other versions)

Classifications

    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies
    • Y02T50/67—Relevant aircraft propulsion technologies
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/78—Other construction of jet pipes

Similar Documents

Publication Publication Date Title
Marshall et al. A chief engineer's view of the NASA X-43A scramjet flight test
Engelund et al. Propulsion system airframe integration issues and aerodynamic database development for the Hyper-X flight research vehicle
Abdol-Hamid et al. Overview of Ares-I CFD ascent aerodynamic data development and analysis based on USM3D
Orme et al. Selected performance measurements of the F-15 ACTIVE axisymmetric thrust-vectoring nozzle
Martens F-15 Nozzle/afterbody integration
Garg Aircraft engine advanced controls research under NASA aeronautics research mission programs
McClinton et al. Wind tunnel testing, flight scaling and flight validation with Hyper-X
Southwick et al. High stability engine control (HISTEC) flight test results
Orme et al. Initial flight test evaluation of the F-15 ACTIVE axisymmetric vectoring nozzle performance
Howe et al. Quiet Spike Near Field Flight Test Pressure Measurements with CFD Comparisons
Burcham, Jr et al. Propulsion flight research at NASA Dryden from 1967 to 1997
Deere Experimental and Computational Investigation of a Translating-Throat Single-Expansion-Ramp Nozzle
Johnson Aircraft Ground Tests and Subscale Model Results of Axial Thrust Loss Caused by Thrust Vectoring Using Turning Vanes
Gallagher Investigation of a Digital Simulation of the XB-70 Inlet and Its Application to Flight-experienced Free-stream Disturbances at Mach Numbers of 2.4 to 2.6
Ellis et al. Beechjet flight test data gathering and level-D simulator aerodynamic mathematical model development
Foster et al. Controls for Agility Research in the NASA High-Alpha Technology Program
Moes et al. Flight stability and control and performance results from the Linear Aerospike SR-71 Experiment (LASRE)
Khalid et al. Propulsion system flight test analysis using modeling techniques
Joshi et al. A design approach to integrated flight and propulsion control
BURCHAM, JR et al. Summary of results of NASA F-15 flight research program
Cross Force and Moment Accounting Procedure for Vehicles With Air-Breathing Propulsion Systems
Bowers et al. Throttle Dependent Forces–A Primer
Price An Investigation of F-16 Nozzle-Afterbody Forces at Transonic Mach Numbers with Emphasis on Support System Interference
Burcham Jr et al. An overview of integrated flight-propulsion controls flight research on the NASA F-15 research airplane
Marks et al. Normalization of F/A-18E/F flight demonstrated dynamic minimum control airspeeds to reference conditions