Aerodynamic Characteristics of a Spoiler-slot-deflector Control on a 45© Sweptback Wing at Mach Numbers of 1.61 and 2.01

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ISBN 13 :
Total Pages : 52 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Aerodynamic Characteristics of a Spoiler-slot-deflector Control on a 45© Sweptback Wing at Mach Numbers of 1.61 and 2.01 by : Douglas R. Lord

Download or read book Aerodynamic Characteristics of a Spoiler-slot-deflector Control on a 45© Sweptback Wing at Mach Numbers of 1.61 and 2.01 written by Douglas R. Lord and published by . This book was released on 1957 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been made in the Langley 4- by 4-foot supersonic pressure tunnel at Mach numbers of 1.61 and 2.01 to determine the aerodynamic characteristics of a spoiler-slot-deflector control on a 45 degree sweptback wing having an aspect ratio of 3.5, a taper ratio of 0.3, and an NACA 65A005 airfoil section. The model was equipped with a 15-percent-chord spoiler-slot-deflector extending from 13 o 78 percent of the wing semispan. The spoiler and deflector were hinged along the 60- and 75-percent-chord lines, respectively. Tests were made at a Reynolds number of 3,000,000 (based on the mean aerodynamic chord of the wing) and covered ranges of angles of attack from -3 to 15 degrees, spoiler projections from 0 to 8.0 percent chord, and deflector projections from 0 to 7.6 percent chord.

Aerodynamic Characteristics of a Spoiler-slot-deflector Control on a 45° Sweptback-wing-fuselage Model at High Subsonic Speeds

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ISBN 13 :
Total Pages : 80 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Aerodynamic Characteristics of a Spoiler-slot-deflector Control on a 45° Sweptback-wing-fuselage Model at High Subsonic Speeds by : Alexander D. Hammond

Download or read book Aerodynamic Characteristics of a Spoiler-slot-deflector Control on a 45° Sweptback-wing-fuselage Model at High Subsonic Speeds written by Alexander D. Hammond and published by . This book was released on 1960 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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°

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ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis 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° by : Gerald V. Foster

Download or read book 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° written by Gerald V. Foster and published by . This book was released on 1960 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Characteristics of a Spoiler-slot-deflector Control on a 45 Degree Sweptback Wing at Mach Numbers of 1.61 and 2.01

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ISBN 13 :
Total Pages : 47 pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis Aerodynamic Characteristics of a Spoiler-slot-deflector Control on a 45 Degree Sweptback Wing at Mach Numbers of 1.61 and 2.01 by : Douglas R. Lord

Download or read book Aerodynamic Characteristics of a Spoiler-slot-deflector Control on a 45 Degree Sweptback Wing at Mach Numbers of 1.61 and 2.01 written by Douglas R. Lord and published by . This book was released on 1957 with total page 47 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Characteristics of a Spoiler-slot-deflector Control on a 45 Degree Sweptback-wing-fuselage Model at High Subsonic Speeds

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ISBN 13 :
Total Pages : 76 pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis Aerodynamic Characteristics of a Spoiler-slot-deflector Control on a 45 Degree Sweptback-wing-fuselage Model at High Subsonic Speeds by : Alexander D. Hammond

Download or read book Aerodynamic Characteristics of a Spoiler-slot-deflector Control on a 45 Degree Sweptback-wing-fuselage Model at High Subsonic Speeds written by Alexander D. Hammond and published by . This book was released on 1963 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Pressure Distributions and Aerodynamic Characteristics of Several Spoiler Controls on a 40 Degree Sweptback Wing at a Mach Number of 1.61

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ISBN 13 :
Total Pages : 70 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Pressure Distributions and Aerodynamic Characteristics of Several Spoiler Controls on a 40 Degree Sweptback Wing at a Mach Number of 1.61 by : Emma Jean Landrum

Download or read book Pressure Distributions and Aerodynamic Characteristics of Several Spoiler Controls on a 40 Degree Sweptback Wing at a Mach Number of 1.61 written by Emma Jean Landrum and published by . This book was released on 1960 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Characteristics of Several Jet-spoiler Controls on a 45 Degree Sweptback Wing at Mach Numbers of 1.61 and 2.01

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ISBN 13 :
Total Pages : 93 pages
Book Rating : 4.:/5 (725 download)

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Book Synopsis Aerodynamic Characteristics of Several Jet-spoiler Controls on a 45 Degree Sweptback Wing at Mach Numbers of 1.61 and 2.01 by : Douglas R. Lord

Download or read book Aerodynamic Characteristics of Several Jet-spoiler Controls on a 45 Degree Sweptback Wing at Mach Numbers of 1.61 and 2.01 written by Douglas R. Lord and published by . This book was released on 1958 with total page 93 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been made in the Langley 4- by 4-foot supersonic pressure tunnel at Mach numbers of 1.61 and 2.01 to determine the aerodynamic characteristics of several jet-spoiler controls on a wing having a 45 degree sweepback of the quarter-chord line, an aspect ratio of 3.5, a taper ratio of 0.3, and an NACA 65A005 airfoil section.

Low-speed Investigation of the Lateral-control Characteristics of a Flap-type Spoiler and a Spoiler-slot Deflector on a 30 Degree Sweptback Wing-fuselage Model Having an Aspect Ratio of 3, a Taper Ratio of 0.5, and NACA 65A004 Airfoil Section

Download Low-speed Investigation of the Lateral-control Characteristics of a Flap-type Spoiler and a Spoiler-slot Deflector on a 30 Degree Sweptback Wing-fuselage Model Having an Aspect Ratio of 3, a Taper Ratio of 0.5, and NACA 65A004 Airfoil Section PDF Online Free

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ISBN 13 :
Total Pages : 25 pages
Book Rating : 4.:/5 (722 download)

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Book Synopsis Low-speed Investigation of the Lateral-control Characteristics of a Flap-type Spoiler and a Spoiler-slot Deflector on a 30 Degree Sweptback Wing-fuselage Model Having an Aspect Ratio of 3, a Taper Ratio of 0.5, and NACA 65A004 Airfoil Section by : Alexander D. Hammond

Download or read book Low-speed Investigation of the Lateral-control Characteristics of a Flap-type Spoiler and a Spoiler-slot Deflector on a 30 Degree Sweptback Wing-fuselage Model Having an Aspect Ratio of 3, a Taper Ratio of 0.5, and NACA 65A004 Airfoil Section written by Alexander D. Hammond and published by . This book was released on 1956 with total page 25 pages. Available in PDF, EPUB and Kindle. Book excerpt: A wind-tunnel investigation has been made at low speed in the Langley 300 MPH 7- by 10-foot tunnel to determine the effect of deflector projection on the control effectiveness of spoiler-slot-deflectors on a 30 degree sweptback wing-fuselage model equipped with either a 15-percent-chord spoiler or a spoiler-slot-deflector that extended from the 20- to the 99-percent-semispan station of the right ring. The wing had an aspect ratio of 3, a taper ratio of 0.5, and NACA 65A004 airfoil section. The tests were made at angles of attack from -4 to 24 degrees at Mach number of 0.26 for control projections from 0 to 12 percent chord. The deflector of the spoiler-slot-deflector configuration was tested at projections from zero to a projection equal to the spoiler projection at each spoiler projection.

Pressure Distributions and Aerodynamic Characteristics of Several Spoiler Controls on a 40° Sweptback Wing at a Mach Number of 1.61

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ISBN 13 :
Total Pages : 66 pages
Book Rating : 4.:/5 (25 download)

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Book Synopsis Pressure Distributions and Aerodynamic Characteristics of Several Spoiler Controls on a 40° Sweptback Wing at a Mach Number of 1.61 by : Emma Jean Landrum

Download or read book Pressure Distributions and Aerodynamic Characteristics of Several Spoiler Controls on a 40° Sweptback Wing at a Mach Number of 1.61 written by Emma Jean Landrum and published by . This book was released on 1960 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Transonic Wind-tunnel Investigation of the Effect of Control Span and Large Wing-tip Nacelles on Effectiveness of Spoiler-slot- Deflector Controls on an Unswept-wing Fighter-type Airplane

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ISBN 13 :
Total Pages : 34 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Transonic Wind-tunnel Investigation of the Effect of Control Span and Large Wing-tip Nacelles on Effectiveness of Spoiler-slot- Deflector Controls on an Unswept-wing Fighter-type Airplane by :

Download or read book Transonic Wind-tunnel Investigation of the Effect of Control Span and Large Wing-tip Nacelles on Effectiveness of Spoiler-slot- Deflector Controls on an Unswept-wing Fighter-type Airplane written by and published by . This book was released on 1960 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Pressure Distributions and Aerodynamic Characteristics of Several Spoiler-type Controls on a Trapezoidal Wing at Mach Numbers of 1.61 and 2.01

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ISBN 13 :
Total Pages : 169 pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis Pressure Distributions and Aerodynamic Characteristics of Several Spoiler-type Controls on a Trapezoidal Wing at Mach Numbers of 1.61 and 2.01 by : Douglas R. Lord

Download or read book Pressure Distributions and Aerodynamic Characteristics of Several Spoiler-type Controls on a Trapezoidal Wing at Mach Numbers of 1.61 and 2.01 written by Douglas R. Lord and published by . This book was released on 1956 with total page 169 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Free-flight Measurements of the Rolling Effectiveness and Drag of Trailing-edge Spoilers on a Tapered Sweptback Wing at Mach Numbers Between 0.6 and 1.4

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ISBN 13 :
Total Pages : 18 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Free-flight Measurements of the Rolling Effectiveness and Drag of Trailing-edge Spoilers on a Tapered Sweptback Wing at Mach Numbers Between 0.6 and 1.4 by : Eugene D. Schult

Download or read book Free-flight Measurements of the Rolling Effectiveness and Drag of Trailing-edge Spoilers on a Tapered Sweptback Wing at Mach Numbers Between 0.6 and 1.4 written by Eugene D. Schult and published by . This book was released on 1954 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Load Distribution Over a 45 Degree Swept Wing Having a Spoiler-slot-deflector Aileron and Other Spoiler Ailerons for Mach Numbers from 0.60 to 1.03

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ISBN 13 :
Total Pages : 118 pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis Aerodynamic Load Distribution Over a 45 Degree Swept Wing Having a Spoiler-slot-deflector Aileron and Other Spoiler Ailerons for Mach Numbers from 0.60 to 1.03 by : F.E. Jr West

Download or read book Aerodynamic Load Distribution Over a 45 Degree Swept Wing Having a Spoiler-slot-deflector Aileron and Other Spoiler Ailerons for Mach Numbers from 0.60 to 1.03 written by F.E. Jr West and published by . This book was released on 1957 with total page 118 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Results of an Investigation at High Subsonic Speeds to Determine Lateral-control and Hinge-moment Characteristics of a Spoiler-slot-deflector Configuration on a 35 Degree Sweptback Wing

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ISBN 13 :
Total Pages : 80 pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis Results of an Investigation at High Subsonic Speeds to Determine Lateral-control and Hinge-moment Characteristics of a Spoiler-slot-deflector Configuration on a 35 Degree Sweptback Wing by : Alexander D. Hammond

Download or read book Results of an Investigation at High Subsonic Speeds to Determine Lateral-control and Hinge-moment Characteristics of a Spoiler-slot-deflector Configuration on a 35 Degree Sweptback Wing written by Alexander D. Hammond and published by . This book was released on 1957 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Effects of Wing and Tail Location on the Aerodynamic Characteristics of an Airplane for Mach Numbers from 0.25 to 4.63

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ISBN 13 :
Total Pages : 34 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Effects of Wing and Tail Location on the Aerodynamic Characteristics of an Airplane for Mach Numbers from 0.25 to 4.63 by :

Download or read book Effects of Wing and Tail Location on the Aerodynamic Characteristics of an Airplane for Mach Numbers from 0.25 to 4.63 written by and published by . This book was released on 1983 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Characteristics of a Full-span Trailing-edge Control on a 60 Degree Delta Wing with and Without a Spoiler at Mach Number 1.61

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ISBN 13 :
Total Pages : 49 pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis Aerodynamic Characteristics of a Full-span Trailing-edge Control on a 60 Degree Delta Wing with and Without a Spoiler at Mach Number 1.61 by : Douglas R. Lord

Download or read book Aerodynamic Characteristics of a Full-span Trailing-edge Control on a 60 Degree Delta Wing with and Without a Spoiler at Mach Number 1.61 written by Douglas R. Lord and published by . This book was released on 1954 with total page 49 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Load Distribution on a 45 Degree Sweptback Wing with Leading-edge Chord-extensions at Transonic Speeds, Including Effects of a Spoiler-slot-deflector Aileron

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ISBN 13 :
Total Pages : 78 pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis Aerodynamic Load Distribution on a 45 Degree Sweptback Wing with Leading-edge Chord-extensions at Transonic Speeds, Including Effects of a Spoiler-slot-deflector Aileron by : James W. Schmeer

Download or read book Aerodynamic Load Distribution on a 45 Degree Sweptback Wing with Leading-edge Chord-extensions at Transonic Speeds, Including Effects of a Spoiler-slot-deflector Aileron written by James W. Schmeer and published by . This book was released on 1958 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt: