Force Tests Results for Body-mounted Lateral Controls and Speed Brakes on a 45 Degree Swept-wing Model at Mach Numbers from 0.80 to 0.98 PDF Download

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Force Tests Results for Body-mounted Lateral Controls and Speed Brakes on a 45 Degree Swept-wing Model at Mach Numbers from 0.80 to 0.98

Force Tests Results for Body-mounted Lateral Controls and Speed Brakes on a 45 Degree Swept-wing Model at Mach Numbers from 0.80 to 0.98 PDF Author: F. E. West
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 32

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Book Description
An investigation has been made in the Langley 16-foot transonic tunnel to determine the aerodynamic characteristics of several body-mounted lateral-control and speed-brake configurations. The basic model had a 45 degree swept wing with an aspect ratio of 3. Six-component balance data were obtained at Mach numbers of 0.80, 0.94, and 0.98 for angles of attack that usually ranged from about zero to 21 degrees.

Force Tests Results for Body-mounted Lateral Controls and Speed Brakes on a 45 Degree Swept-wing Model at Mach Numbers from 0.80 to 0.98

Force Tests Results for Body-mounted Lateral Controls and Speed Brakes on a 45 Degree Swept-wing Model at Mach Numbers from 0.80 to 0.98 PDF Author: F. E. West
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 32

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Book Description
An investigation has been made in the Langley 16-foot transonic tunnel to determine the aerodynamic characteristics of several body-mounted lateral-control and speed-brake configurations. The basic model had a 45 degree swept wing with an aspect ratio of 3. Six-component balance data were obtained at Mach numbers of 0.80, 0.94, and 0.98 for angles of attack that usually ranged from about zero to 21 degrees.

Force Test Results for Body-mounted Lateral Controls and Speed Brakes on a 45° Swept-wing Model at Mach Numbers from 0.80 to 0.98

Force Test Results for Body-mounted Lateral Controls and Speed Brakes on a 45° Swept-wing Model at Mach Numbers from 0.80 to 0.98 PDF Author: F. E. West
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 32

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Book Description

Effect of Body-mounted Lateral Controls and Speed Brakes on the Aerodynamic Load Distribution Over a 45 Degree Swept Wing at Mach Numbers from 0.80 to 0.98

Effect of Body-mounted Lateral Controls and Speed Brakes on the Aerodynamic Load Distribution Over a 45 Degree Swept Wing at Mach Numbers from 0.80 to 0.98 PDF Author: F. E. West
Publisher:
ISBN:
Category :
Languages : en
Pages : 76

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Book Description

Effect of Body-Mounted Lateral Controls and Speed Brakes on the Aerodynamic Load Distribution Over a 45 Deg Swept Wing at Mach Numbers from 0.80 to 0.98

Effect of Body-Mounted Lateral Controls and Speed Brakes on the Aerodynamic Load Distribution Over a 45 Deg Swept Wing at Mach Numbers from 0.80 to 0.98 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 80

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Book Description

Effect of Body-mounted Lateral Controls and Speed Brakes on the Aerodynamic Load Distribution Over a 45 Degree Swept Wing at Mach Numbers from 0.80 to 0.98

Effect of Body-mounted Lateral Controls and Speed Brakes on the Aerodynamic Load Distribution Over a 45 Degree Swept Wing at Mach Numbers from 0.80 to 0.98 PDF Author: F. E. West
Publisher:
ISBN:
Category :
Languages : en
Pages : 0

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Book Description

Effect of Body-mounted Lateral Controls and Speed Brakes on the Aerodynamic Load Distribution Over a 45° Swept Wing at Mach Numbers from 0.80 to 0.98

Effect of Body-mounted Lateral Controls and Speed Brakes on the Aerodynamic Load Distribution Over a 45° Swept Wing at Mach Numbers from 0.80 to 0.98 PDF Author: F. E. West
Publisher:
ISBN:
Category :
Languages : en
Pages : 72

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Book Description

Beyond Tube-and-Wing

Beyond Tube-and-Wing PDF Author: Bruce Larrimer
Publisher:
ISBN: 9781626830592
Category :
Languages : en
Pages :

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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°

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° PDF Author: Gerald V. Foster
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 38

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Book Description

Introduction to Aircraft Flight Mechanics

Introduction to Aircraft Flight Mechanics PDF Author: Thomas R. Yechout
Publisher: AIAA
ISBN: 9781600860782
Category : Aerodynamics
Languages : en
Pages : 666

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Book Description
Based on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.

Static Lateral Stability and Control Characteristics of a Model of a 45 Degree Swept-wing Fighter Airplane with Various Vertical Tails at Mach Numbers of 1.41, 1.61, and 2.01

Static Lateral Stability and Control Characteristics of a Model of a 45 Degree Swept-wing Fighter Airplane with Various Vertical Tails at Mach Numbers of 1.41, 1.61, and 2.01 PDF Author: M. Leroy Spearman
Publisher:
ISBN:
Category :
Languages : en
Pages : 49

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Book Description