Longitudinal Aerodynamic Characteristics of Several Thick-slab Delta Wings at Mach Numbers of 3.00, 4.50, and 6.00 and Angles of Attack to 95 Deg

Longitudinal Aerodynamic Characteristics of Several Thick-slab Delta Wings at Mach Numbers of 3.00, 4.50, and 6.00 and Angles of Attack to 95 Deg PDF Author:
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Languages : en
Pages : 76

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The Aerodynamic Characteristics of Several Thick Delta Wings at Mach Numbers to 6 and Angles of Attack 50 Deg

The Aerodynamic Characteristics of Several Thick Delta Wings at Mach Numbers to 6 and Angles of Attack 50 Deg PDF Author:
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Category :
Languages : en
Pages : 108

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The Aerodynamic Characteristics of Several Thick Delta Wings at Mach Numbers to 6 and Angles of Attack 50°

The Aerodynamic Characteristics of Several Thick Delta Wings at Mach Numbers to 6 and Angles of Attack 50° PDF Author: John B. McDevitt
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Category : Aerodynamics
Languages : en
Pages : 114

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Comparison of Longitudinal Aerodynamic Characteristics of Curved and Straight Leading-edge Delta Wings at Mach Numbers 3 and 6

Comparison of Longitudinal Aerodynamic Characteristics of Curved and Straight Leading-edge Delta Wings at Mach Numbers 3 and 6 PDF Author: Dewey E. Wornom
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Category : Delta wing airplanes
Languages : en
Pages : 30

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The Effects of Fuselage Size on the Low-speed Longitudinal Aerodynamic Characteristics of a Thin 60© Delta Wing with and Without a Double Slotted Flap

The Effects of Fuselage Size on the Low-speed Longitudinal Aerodynamic Characteristics of a Thin 60© Delta Wing with and Without a Double Slotted Flap PDF Author: John M. Riebe
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Category : Airplanes
Languages : en
Pages : 32

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Aerodynamic Characteristics of Two Delta Wings and Two Trapezoidal Wings at Mach Number of 4.04

Aerodynamic Characteristics of Two Delta Wings and Two Trapezoidal Wings at Mach Number of 4.04 PDF Author: Robert W. Dunning
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Category : Airplanes
Languages : en
Pages : 24

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Characteristics at Mach Number of 2.03 of a Series of Wings Having Various Spanwise Distributions of Thickness Ration and Chord

Characteristics at Mach Number of 2.03 of a Series of Wings Having Various Spanwise Distributions of Thickness Ration and Chord PDF Author: A. Warner Robins
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Category :
Languages : en
Pages : 30

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A Note on the Drag Due to Lift of Delta Wings at Mach Numbers Up to 2.0

A Note on the Drag Due to Lift of Delta Wings at Mach Numbers Up to 2.0 PDF Author: Robert S. Osborne
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Category : Aerodynamics
Languages : en
Pages : 20

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Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2.20 of a Model of an 82 Deg Delta Wing Airplane Having Auxiliary Variable-sweep Wing Panels

Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2.20 of a Model of an 82 Deg Delta Wing Airplane Having Auxiliary Variable-sweep Wing Panels PDF Author:
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Languages : en
Pages : 44

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STATIC LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF SEVERAL WING AND BLUNT-BODY SHAPES APPLICABLE FOR USE AS REENTRY CONFIGURATIONS AT A MACH NUMBER OF 6.8 AND ANGLES OF ATTACK UP TO 90 DEG

STATIC LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF SEVERAL WING AND BLUNT-BODY SHAPES APPLICABLE FOR USE AS REENTRY CONFIGURATIONS AT A MACH NUMBER OF 6.8 AND ANGLES OF ATTACK UP TO 90 DEG PDF Author:
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Languages : en
Pages : 48

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