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

MEYN et al., 1992 - Google Patents

Full-scale high angle-of-attack tests of an F/A-18

MEYN et al., 1992

View PDF
Document ID
9567383016965180317
Author
MEYN L
LANSER W
JAMES K
Publication year
Publication venue
10th Applied Aerodynamics Conference

External Links

Snippet

This paper presents an overview of high angle-ofattack tests of a full-scale FiA-18 in the 80- by 120-Foot Wind Tunnel of the National Full-Scale Aerodynamic Complex at NASA Ames Research Center at Moffett Field, California. A production aircraft was tested over an angle …
Continue reading at www.researchgate.net (PDF) (other versions)

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02—Aircraft characterised by the type or position of power plant
    • B64D27/16—Aircraft characterised by the type or position of power plant of jet type
    • B64D27/18—Aircraft characterised by the type or position of power plant of jet type within or attached to wing
    • 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
    • Y02T50/10—Drag reduction
    • Y02T50/16—Drag reduction by influencing airflow

Similar Documents

Publication Publication Date Title
KR20010071156A (en) Pitot-static tube
MEYN et al. Full-scale high angle-of-attack tests of an F/A-18
Shi et al. Serpentine inlet design and analysis
Murri et al. Actuated forebody strake controls for the F-18 high-alpha research vehicle
Lanser et al. Forebody flow control on a full-scale F/A-18 aircraft
Saltzman Base Pressure Coefficients Obtained From the X-15 Airplane for Mach Numbers up to 6
Chan et al. Transonic drag reduction through trailing-edge blowing on the FAST-MAC circulation control model
Stephen et al. Investigation of Articulating Nosecone for Flight Control Under Mach 2 Conditions
Malcolm et al. Enhanced controllability through vortex manipulation on fighter aircraft at high angles of attack
Hayman et al. Jet Effects on Cylindrical Afterbodies Housing Sonic and Supersonic Nozzles which Exhaust Against a Supersonic Stream at Angles of Attack from 90 ̊to 180 ̊
Spearman et al. Aerodynamics of a sphere and an oblate spheroid for Mach numbers from 0.6 to 10.5 including some effects of test conditions
Watanabe et al. Control of supersonic inlet with variable ramp
Englert et al. Effect of Jet-Nozzle-Expansion Ratio on Drag of Parabolic Afterbodies
HALL et al. Impact of nose-probe chines on the vortex flows about the F-16C
Jischke et al. Experimental surface pressures on cone-derived waveriders for freestream M= 3-5
Hall et al. Evaluation of gritting strategies for high angle of attack using wind tunnel and flight test data for the F/A-18
JAMES, JR Aerodynamics of rocket plume interactions at supersonic speeds
Aley et al. Experimental characterization of a high-lift supercritical airfoil with microjets
Lanser et al. Comparison of full-scale, small-scale, and CFD results for F/A-18 forebody slot blowing
LEE et al. Buffet load measurements on an F/A-18 vertical fin at high-angle-of-attack
HUTCHISON et al. Investigation of advanced thrust vectoring exhaust systems for high speed propulsive lift
Hodgkin et al. Forebody flow control for extended high-angle-of-attack maneuvers
Spreemann Free-Stream Interference Effects on Effectiveness of Control Jets Near the Wing Tip of a VTOL Aircraft Model
Tolhurst et al. Full-scale Wind-tunnel Investigation of the Effects of a Target-type Thrust Reverser on the Low-speed Aerodynamic Characteristics of a Single-engine Jet Airplane
Chanetz et al. Transonic Wind Tunnels