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Low Speed Investigation Of Aileron And Spoiler Characteristics Of A Wing Having 42 Degrees Sweepback Of The Leading Edge And Circular Arc Airfoil Sections At Reynolds Of Approximately 60 X 106
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Book Synopsis Low-speed Investigation of Aileron and Spoiler Characteristics of a Wing Having 42 Degrees Sweepback of the Leading Edge and Circular-arc Airfoil Sections at Reynolds of Approximately 6.0 X (10)6 by : Stanley H. Spooner
Download or read book Low-speed Investigation of Aileron and Spoiler Characteristics of a Wing Having 42 Degrees Sweepback of the Leading Edge and Circular-arc Airfoil Sections at Reynolds of Approximately 6.0 X (10)6 written by Stanley H. Spooner and published by . This book was released on 1949 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Low-speed Lateral Stability and Aileron-effectiveness Characteristics at a Reynolds Number of 3.5 X (10)6 of a Wing with Leading-edge Sweepback Decreasing from 45 Degrees at the Root to 20 Degrees at the Tip by : Roy H. Lange
Download or read book Low-speed Lateral Stability and Aileron-effectiveness Characteristics at a Reynolds Number of 3.5 X (10)6 of a Wing with Leading-edge Sweepback Decreasing from 45 Degrees at the Root to 20 Degrees at the Tip written by Roy H. Lange and published by . This book was released on 1950 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of Low-speed Aileron Control Characteristics at a Reynolds Number of 6,800,000 of a Wing with Leading Edge Swept Back 42 Degrees with and Without High-lift Devices by : Thomas V. Bollech
Download or read book Investigation of Low-speed Aileron Control Characteristics at a Reynolds Number of 6,800,000 of a Wing with Leading Edge Swept Back 42 Degrees with and Without High-lift Devices written by Thomas V. Bollech and published by . This book was released on 1949 with total page 31 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Low-speed Investigation of the Effect of Several Flap and Spoiler Ailerons on the Lateral Characteristics of a 47.5 Degrees Sweptback-wing - Fuselage Combination at a Reynolds Number of 4.4 X (10)6 by : Jerome Pasamanick
Download or read book Low-speed Investigation of the Effect of Several Flap and Spoiler Ailerons on the Lateral Characteristics of a 47.5 Degrees Sweptback-wing - Fuselage Combination at a Reynolds Number of 4.4 X (10)6 written by Jerome Pasamanick and published by . This book was released on 1950 with total page 57 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Low-speed Lateral-control Characteristics of an Unswept Wing with Hexagonal Airfoil Sections and Aspect Ratio 2.5 Equipped with Spoilers and with Sharp- and Thickened-trailing-edge Flap-type Ailerons at a Reynolds Number of 7.6 X (10)6 by : James E. Fitzpatrick
Download or read book Low-speed Lateral-control Characteristics of an Unswept Wing with Hexagonal Airfoil Sections and Aspect Ratio 2.5 Equipped with Spoilers and with Sharp- and Thickened-trailing-edge Flap-type Ailerons at a Reynolds Number of 7.6 X (10)6 written by James E. Fitzpatrick and published by . This book was released on 1952 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Low-speed Characteristics in Pitch of a 42 Degrees Sweptback Wing with Aspect Ratio 3.9 and Circular-arc Airfoil Sections by : Robert H. Neely
Download or read book Low-speed Characteristics in Pitch of a 42 Degrees Sweptback Wing with Aspect Ratio 3.9 and Circular-arc Airfoil Sections written by Robert H. Neely and published by . This book was released on 1947 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Low-speed Lateral-control Investigation of a Flap-type Spoiler Aileron with and Without a Deflector and Slot on a 6-percent-thick, Tapered, 45 Degree Sweptback Wing of Aspect Ratio 4 by : James M. Watson
Download or read book Low-speed Lateral-control Investigation of a Flap-type Spoiler Aileron with and Without a Deflector and Slot on a 6-percent-thick, Tapered, 45 Degree Sweptback Wing of Aspect Ratio 4 written by James M. Watson and published by . This book was released on 1952 with total page 11 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been made in the Langley 300 MPH 7- by 10-foot tunnel to determine the lateral control characteristics of a deflector and slot arrangement in conjunction with a flap-type spoiler aileron. The wing had a sweepback of 45 degrees at the quarter-chord line, an aspect ratio of 4, a taper ratio of 0.6, and an NACA 65A006 airfoil section parallel to the free air stream.
Book Synopsis Low-speed Pressure Distributions Over the Drooped-nose Flap of a 42 Degree Sweptback Wing with Circular-arc Airfoil Sections at a Reynolds Number of 5.3 X (10)6 by : Stanley H. Spooner
Download or read book Low-speed Pressure Distributions Over the Drooped-nose Flap of a 42 Degree Sweptback Wing with Circular-arc Airfoil Sections at a Reynolds Number of 5.3 X (10)6 written by Stanley H. Spooner and published by . This book was released on 1948 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation at High Subsonic Speeds of the Lateral-control Characteristics of an Aileron and a Stepped Spoiler on a Wing with Leading Edge Swept Back 51.3 Degrees by : Leslie E. Schneiter
Download or read book Wind-tunnel Investigation at High Subsonic Speeds of the Lateral-control Characteristics of an Aileron and a Stepped Spoiler on a Wing with Leading Edge Swept Back 51.3 Degrees written by Leslie E. Schneiter and published by . This book was released on 1949 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: A wind-tunnel investigation has been made through a speed range from a Mach number of approximately 0.90 to determine the lateral-control characteristics of a 2-percent-chord by 39-percent-semispan aileron and a 60-percent-semispan stepped spoiler on a semispan-wing model with aspect ratio of 3.06 having 51.3 degree sweepback of the wing leading edge. In addition, the aerodynamic characteristics of the plain wing were determined through the speed range.
Book Synopsis Low-Speed Characteristics in Pitch of a 42 Degree Swept-Back Wing with Aspect Ratio 3.9 and Circular-Arc Airfoil Sections by :
Download or read book Low-Speed Characteristics in Pitch of a 42 Degree Swept-Back Wing with Aspect Ratio 3.9 and Circular-Arc Airfoil Sections written by and published by . This book was released on 1947 with total page 57 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Low-speed Longitudinal Characteristics of a Circular-arc 52 Degrees Sweptback Wing of Aspect Ratio 2.84 with and Without Leading-edge and Trailing-edge Flaps at Reynolds Number from 1.6 X (10)6 to 9.7 X (10)6 by : Gerald V. Foster
Download or read book Low-speed Longitudinal Characteristics of a Circular-arc 52 Degrees Sweptback Wing of Aspect Ratio 2.84 with and Without Leading-edge and Trailing-edge Flaps at Reynolds Number from 1.6 X (10)6 to 9.7 X (10)6 written by Gerald V. Foster and published by . This book was released on 1950 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Maximum-lift Characteristics of a Wing with the Leading-edge Sweepback Decreasing from 45 Degrees at the Root to 20 Degrees at the Tip at Reynolds Numbers from 2.4 X 106 to 6.0 X 106 by : Roy H. Lange
Download or read book Maximum-lift Characteristics of a Wing with the Leading-edge Sweepback Decreasing from 45 Degrees at the Root to 20 Degrees at the Tip at Reynolds Numbers from 2.4 X 106 to 6.0 X 106 written by Roy H. Lange and published by . This book was released on 1951 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Comparison of Semispan and Full-span Tests of A 47.5 Degrees Sweptback Wing with Symmetrical Circular-arc Sections and Having Drooped-nose Flaps, Trailing-edge Flaps, and Ailerons by : Stanley Lipson
Download or read book Comparison of Semispan and Full-span Tests of A 47.5 Degrees Sweptback Wing with Symmetrical Circular-arc Sections and Having Drooped-nose Flaps, Trailing-edge Flaps, and Ailerons written by Stanley Lipson and published by . This book was released on 1951 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was conducted in the Langley full-scale tunnel to determine the comparative characteristics of a full-span and semispan 47.5 degrees sweptback wing having 10-percent thick biconvex airfoil sections and an aspect ratio of 3.5. The configurations tested were the basic wing, the wing with various combinations of leading- and trailing edge flaps, and the basic wing with an aileron deflection. The results included both force and pressure measurements and were obtained at a Reynolds number of 4,200,000 and a Mach number of 0.07.
Book Synopsis Low-speed Longitudinal and Wake Air-flow Characteristics at a Reynolds Number of 5.5 X (10)6 of a Circular-arc 52 Degree Sweptback Wing with a Fuselage and a Horizontal Tail at Various Vertical Positions by : Gerald V. Foster
Download or read book Low-speed Longitudinal and Wake Air-flow Characteristics at a Reynolds Number of 5.5 X (10)6 of a Circular-arc 52 Degree Sweptback Wing with a Fuselage and a Horizontal Tail at Various Vertical Positions written by Gerald V. Foster and published by . This book was released on 1951 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Maximum-lift Characteristics of a Wing with the Leading-edge Sweepback Decreasing from 45 Degrees at the Root to 20 Degrees at the Tip at Reynolds Numbers from 2.4 X (10)6 to 6.0 X (10)6 by : Roy H. Lange
Download or read book Maximum-lift Characteristics of a Wing with the Leading-edge Sweepback Decreasing from 45 Degrees at the Root to 20 Degrees at the Tip at Reynolds Numbers from 2.4 X (10)6 to 6.0 X (10)6 written by Roy H. Lange and published by . This book was released on 1950 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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:
