Related Books

An Investigation of Wing and Aileron Loads Due to Deflected Inboard and Outboard Ailerons on a 4-percent-thick 30 Degree Swepptback Wing at Transonic Speeds
Language: en
Pages: 286

An Investigation of Wing and Aileron Loads Due to Deflected Inboard and Outboard Ailerons on a 4-percent-thick 30 Degree Swepptback Wing at Transonic Speeds

Authors: Charles F. Whitcomb
Categories:
Type: BOOK - Published: 1961 - Publisher:

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Investigation at Transonic Speeds of Loading Over a 30 Deg Sweptback Wing of Aspect Ratio 3, Taper Ratio 0.2, and NACA 65A004 Airfoil Section Mounted on a Body
Language: en
Pages: 88

Investigation at Transonic Speeds of Loading Over a 30 Deg Sweptback Wing of Aspect Ratio 3, Taper Ratio 0.2, and NACA 65A004 Airfoil Section Mounted on a Body

Authors: Donald D. Arabian
Categories: Aerodynamics, Transonic
Type: BOOK - Published: 1960 - Publisher:

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The aerodynamic load characteristics of a wing-body combination were determined experimentally at Mach numbers from 0.80 to 1.03 for angles of attack up to 26 d
Loads on Thin Wings at Transonic Speeds
Language: en
Pages: 22

Loads on Thin Wings at Transonic Speeds

Authors: Don D. Davis (Jr.)
Categories: Aerodynamics, Transonic
Type: BOOK - Published: 1955 - Publisher:

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A 1-foot Hypervelocity Shock Tunnel in which High-enthalpy, Real-gas Air Flows Can be Generated with Flow Times of about 180 Milliseconds
Language: en
Pages: 48

A 1-foot Hypervelocity Shock Tunnel in which High-enthalpy, Real-gas Air Flows Can be Generated with Flow Times of about 180 Milliseconds

Authors: Bernard E. Cunningham
Categories: Aerodynamics
Type: BOOK - Published: 1962 - Publisher:

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An Investigation at Transonic Speeds of the Effects of Thickness Ratio and of Thickened Root Sections on the Aerodynamic Characteristics of Wings with 47© Sweepback, Aspect Ratio 3.5, and Taper Ratio 0.2 in the Slotted Test Section of the Langley 8-foot High-speed Tunnel
Language: en
Pages: 44

An Investigation at Transonic Speeds of the Effects of Thickness Ratio and of Thickened Root Sections on the Aerodynamic Characteristics of Wings with 47© Sweepback, Aspect Ratio 3.5, and Taper Ratio 0.2 in the Slotted Test Section of the Langley 8-foot High-speed Tunnel

Authors: Ralph P. Bielat
Categories: Aerodynamics, Transonic
Type: BOOK - Published: 1951 - Publisher:

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Four wing-body combinations of the same plan form (47 degree sweep, 3.5 aspect ratio, and 0.2 taper ratio) were compared at transonic speeds in the Langley 8-fo