[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

Foster, 1960 - Google Patents

Stability and Control Characteristics at Mach Numbers of 2.50, 3.00, and 3.71 of a Variable-Wing-Sweep Configuration With Outboard Wing Panels Swept Back 75

Foster, 1960

View HTML
Document ID
15141152811885705606
Author
Foster G
Publication year

External Links

Snippet

An investigation has been conducted in the Langley Unitary Plan wind tunnel at Mach numbers of 2.50, 3.00, and 3.71 to determine the static longitudinal and lateral stability and control characteristics of a variable-wing-sweep configuration with the outboard wing panels …
Continue reading at books.google.com (HTML) (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
    • Y02T50/10—Drag reduction
    • Y02T50/16—Drag reduction by influencing airflow
    • Y02T50/162—Wing tip vortex reduction
    • Y02T50/164—Winglets
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air-flow over aircraft surfaces, not otherwise provided for
    • B64C23/06—Influencing air-flow over aircraft surfaces, not otherwise provided for by generating vortices
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/10—Shape of wings

Similar Documents

Publication Publication Date Title
Foster Stability and Control Characteristics at Mach Numbers of 2.50, 3.00, and 3.71 of a Variable-Wing-Sweep Configuration With Outboard Wing Panels Swept Back 75
Alford et al. An Exploratory Investigation of the Low-Speed Aerodynamic Characteristics of Variable-Wing-Sweep Airplane Configurations
Alford et al. Wind-tunnel studies at subsonic and transonic speeds of a multiple-mission variable-wing-sweep airplane configuration
Parlett et al. Wind-tunnel investigation of a jet transport airplane configuration with high thrust-weight ratio and an external-flow jet flap
Spearman et al. Stability and Control Characteristics at a Mach Number of 2.01 of a Variable-Wing-Sweep Configuration With Outboard Wing Panels Swept Back 75
Foster Effects of Spoiler-slot-deflector Control on the Aerodynamic Characteristics at a Mach Number of 2.01 of a Variable-wing-sweep Configuration with the Outer Wing Panels Swept Back 75°
Morris et al. Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2.20 of a V/STOL Airplane Configuration With a Variable-Sweep Wing and With a Skewed Wing Design
Robinson et al. Stability and Control Characteristics at a Mach Number of 1.41 of a Variable-Sweep Airplane Configuration Capable of Low-Level Supersonic Attack-Outer Wing Swept 75 and 108
Freeman Jr et al. Wind-tunnel investigation of a jet transport airplane configuration with an external-flow jet flap and inboard pod-mounted engines
Foster et al. Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2.20 of a Variable-Wing-Sweep STOL Configuration
Foster et al. Stability and Control Characteristics at a Mach Number of 1.97 of an Airplane Configuration Having Two Types of Variable-Sweep Wings
Putnam Static Longitudinal Aerodynamic Characteristics at a Mach Number of 10.03 of Low-Aspect-Ratio Wing-Body Configurations Suitable for Reentry
Spearman et al. Longitudinal Stability and Control Characteristics at Mach Numbers of 1.41 and 2.01 of a 67 Degree Swept-wing Airplane Configuration with Canard Control Surfaces
Spearman et al. Effects of Canard Surface Size on Stability and Control Characteristics of Two Canard Airplane Configurations at Mach Numbers of 1.41 and 2.01
Smith Wind-Tunnel Investigation at Subsonic and Supersonic Speeds of a Fighter Model Employing a Low-Aspect-Ratio Unswept Wing and a Horizontal Tail Mounted Well Above the Wing Plane-Longitudinal Stability and Control
Foster Sideslip Characteristics at Various Angles of Attack for Several Hypersonic Missile Configurations with Canard Controls at a Mach Number of 2.01
Foster et al. Aerodynamic Characteristics in Pitch at a Mach Number of 1.97 of Two Variable-Wing-Sweep V/STOL Configurations With Outboard Wing Panels Swept Back 75
Henderson The effect of canard and vertical tails on the aerodynamic characteristics of a model with a 59 deg sweptback wing at a Mach number of 0.30
Ware Low-Subsonic-Speed Static Stability of Right-Triangular-Pyramid and Half-Cone Lifting Reentry Configurations
Spearman Investigation of the Aerodynamic Characteristics in Pitch and Sideslip of a 45© Swept-wing Airplane Configuration with Various Vertical Locations of the Wing and Horizontal Tail: Static Lateral and Directional Stability; Mach Numbers of 1.41 and 2.01
Sleeman et al. Low-Speed Effects of High-Lift Devices on the Aerodynamic Characteristics of a Supersonic Transport Model With Outboard Tails
Vogler Wind-tunnel investigation at high subsonic speeds of spoilers of large projection on an NACA 65A006 wing with quarter-chord line swept back 32.6 degrees
Foster et al. Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.20 of a V/STOL airplane configuration with a variable-sweep wing and with a skewed wing design
Goodman et al. Low-Speed Pitching Derivatives of Low-Aspect-Ratio Wings of Triangular and Modified Triangular Plan Forms
MacLeod A Preliminary Low-Speed Wind-Tunnel Investigation of a Thin Delta Wing Equipped With a Double and a Single Slotted Flap