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 PDF Download

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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

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 PDF Author: Charles F. Whitcomb
Publisher:
ISBN:
Category :
Languages : en
Pages : 286

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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

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 PDF Author: Charles F. Whitcomb
Publisher:
ISBN:
Category :
Languages : en
Pages : 286

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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

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 PDF Author: Donald D. Arabian
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 88

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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 degrees. Two wings, both with 30 degrees sweep of the quarter-chord line, taper ratio of 0.2, aspect ratio of 3, and thickness of 4 percent chord, but of different types of construction, were tested. One wing was of solid steel and the other was of plastic with an inner steel core ...

Loads on Thin Wings at Transonic Speeds

Loads on Thin Wings at Transonic Speeds PDF Author: Don D. Davis (Jr.)
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 22

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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

A 1-foot Hypervelocity Shock Tunnel in which High-enthalpy, Real-gas Air Flows Can be Generated with Flow Times of about 180 Milliseconds PDF Author: Bernard E. Cunningham
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 48

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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

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 PDF Author: Ralph P. Bielat
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 44

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Book Description
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-foot high-speed tunnel. Three wings were 4, 6, and 9 percent thick; the fourth was 6 percent thick but, on the inner 0.4 span, tapered to 12-percent thickness at the roots.

Apollo Program Summary Report

Apollo Program Summary Report PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 526

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The Twisting Effect at Transonic Speeds of Spoiler Ailerons on a 45© Sweptback, Aspect-ratio-4, Tapered Wing

The Twisting Effect at Transonic Speeds of Spoiler Ailerons on a 45© Sweptback, Aspect-ratio-4, Tapered Wing PDF Author: Alexander D. Hammond
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 26

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The Apollo Spacecraft: Ertel, I. D. and Morse, M. L. Through November 7, 1962

The Apollo Spacecraft: Ertel, I. D. and Morse, M. L. Through November 7, 1962 PDF Author: Ivan D. Ertel
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 292

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Aerodynamic Characteristics of Low-aspect-ratio Wings in Close Proximity to the Ground

Aerodynamic Characteristics of Low-aspect-ratio Wings in Close Proximity to the Ground PDF Author: Marvin P. Fink
Publisher:
ISBN:
Category :
Languages : en
Pages : 44

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Flight Investigation of an Aileron and a Spoiler on a Wing of the X-3 Airplane Plan Form at Mach Numbers from 0.5 to 1.6

Flight Investigation of an Aileron and a Spoiler on a Wing of the X-3 Airplane Plan Form at Mach Numbers from 0.5 to 1.6 PDF Author: Roland D. English
Publisher:
ISBN:
Category : Ailerons
Languages : en
Pages : 20

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