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Aerodynamic Characteristics Of Four Wings Of Sweepback Angles 0 Degrees 35 Degrees 45 Degrees And 60 Degrees Naca 65a006 Airfoil Section Aspect Ratio 4 And Taper Ratio 06 In Combination With A Fuselage At High Subsonic Mach Numbers And At A Mach Number Of 12
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Book Synopsis Aerodynamic Characteristics of Four Wings of Sweepback Angles 0 Degrees, 35 Degrees, 45 Degrees, and 60 Degrees, NACA 65A006 Airfoil Section, Aspect Ratio 4, and Taper Ratio 0.6 in Combination with a Fuselage at High Subsonic Mach Numbers and at a Mach Number of 1.2 by : Arvo A. Luoma
Download or read book Aerodynamic Characteristics of Four Wings of Sweepback Angles 0 Degrees, 35 Degrees, 45 Degrees, and 60 Degrees, NACA 65A006 Airfoil Section, Aspect Ratio 4, and Taper Ratio 0.6 in Combination with a Fuselage at High Subsonic Mach Numbers and at a Mach Number of 1.2 written by Arvo A. Luoma and published by . This book was released on 1951 with total page 59 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics at a Mach Number of 1.38 of Four Wings of Aspect Ratio 4 Having Quarter-chord Sweep Angles of 0 Degrees, 35 Degrees, 45 Degrees and 60 Degrees by : William B. Jr Kemp
Download or read book Aerodynamic Characteristics at a Mach Number of 1.38 of Four Wings of Aspect Ratio 4 Having Quarter-chord Sweep Angles of 0 Degrees, 35 Degrees, 45 Degrees and 60 Degrees written by William B. Jr Kemp and published by . This book was released on 1950 with total page 41 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of a Wing with Quarter-chord Line Swept Back 35 Degrees, Aspect Ratio 6 , Taper Ratio 0.6, and NACA 65A006 Airfoil Section by : William C. Sleeman
Download or read book Aerodynamic Characteristics of a Wing with Quarter-chord Line Swept Back 35 Degrees, Aspect Ratio 6 , Taper Ratio 0.6, and NACA 65A006 Airfoil Section written by William C. Sleeman and published by . This book was released on 1949 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Studies by : Zbiginew Krzywoblocki
Download or read book Aerodynamic Studies written by Zbiginew Krzywoblocki and published by . This book was released on 1957 with total page 132 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of a Wing with Quarter-chord Line Swept Back 35 Degrees, Aspect Ratio 4, Taper Ratio 0.6, and NACA 65A006 Airfoil Section by : William C. Sleeman
Download or read book Aerodynamic Characteristics of a Wing with Quarter-chord Line Swept Back 35 Degrees, Aspect Ratio 4, Taper Ratio 0.6, and NACA 65A006 Airfoil Section written by William C. Sleeman and published by . This book was released on 1949 with total page 29 pages. Available in PDF, EPUB and Kindle. Book excerpt: This paper presents the results of the investigation of a wing-alone and a wing-fuselage combination employing a wing with the quarter-chord line swept back 35 degrees, aspect ratio 4, taper ratio 0.6, and an NACA 65A006 airfoil section. Lift, drag, pitching moment, and root bending moment were obtained for the wing-alone and wing-body configurations. Effective downwash angles and dynamic-pressure characteristics in the region of a probable tail location were also obtained for these configurations and are presented for a range of tail heights at one tail length. In order to expedite publishing of these data, only a brief analysis is included.
Book Synopsis Aerodynamic Characteristics at Transonic Speeds of a Wing Having a 45 Degree Sweep, Aspect Ratio 8, Taper Ratio 0.45, and Airfoil Sections Varying from the NACA 63A010 Section at the Root to the NACA 63A006 Section at the Tip by : William D. Morrison
Download or read book Aerodynamic Characteristics at Transonic Speeds of a Wing Having a 45 Degree Sweep, Aspect Ratio 8, Taper Ratio 0.45, and Airfoil Sections Varying from the NACA 63A010 Section at the Root to the NACA 63A006 Section at the Tip written by William D. Morrison and published by . This book was released on 1952 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been conducted in the Langley High-Speed 7- by 10-foot tunnel to determine the transonic aerodynamic characteristics of a wing having a spanwise variation in thickness ratio. The wing investigated had 45 degrees of sweepback, aspect ratio 8, taper ratio of 0.45, and airfoil sections tapered from an NACA 63A010 section at the root chord to an NACA 63A006 section at the tip chord. The test Mach number range was from 0.60 to 1.05 at Reynolds numbers of the order of 500,000.
Book Synopsis Aerodynamic Characteristics of a Wing with Quarter-chord Line Swept Back 60 Degrees, Aspect Ratio 4, Taper Ratio 0.6, and NACA 65A006 Airfoil Section - Transonic-bump Method by : Thomas J. Jr King
Download or read book Aerodynamic Characteristics of a Wing with Quarter-chord Line Swept Back 60 Degrees, Aspect Ratio 4, Taper Ratio 0.6, and NACA 65A006 Airfoil Section - Transonic-bump Method written by Thomas J. Jr King and published by . This book was released on 1949 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of a Wing with Quarter-chord Line Swept Back 35 Degrees, Aspect Ratio 4, Taper Ratio 0.6, and NACA 65A006 Aifoil Section - Transonic-bump Method by : William C. Jr Sleeman
Download or read book Aerodynamic Characteristics of a Wing with Quarter-chord Line Swept Back 35 Degrees, Aspect Ratio 4, Taper Ratio 0.6, and NACA 65A006 Aifoil Section - Transonic-bump Method written by William C. Jr Sleeman and published by . This book was released on 1949 with total page 29 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of a Wing with Quarter-chord Line Swept Back 45 Degrees, Aspect Ratio 4, Taper Ratio 0.6, and NACA 65A006 Airfoil Section by : Joseph Weil
Download or read book Aerodynamic Characteristics of a Wing with Quarter-chord Line Swept Back 45 Degrees, Aspect Ratio 4, Taper Ratio 0.6, and NACA 65A006 Airfoil Section written by Joseph Weil and published by . This book was released on 1949 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: As part of an NACA research program, a series of wing-body combinations are being investigated in the Langley high-speed 7- by 10-foot tunnel up to a Mach number of 1.18 utilizing the transonic bump.
Book Synopsis Aerodynamic Characteristics of a 60 Degree Sweptback-wing Airplane Configuration Having Tail Surfaces Located Outboard of the Wing Tips at Mach Numbers of 2.30, 2.97, 3.51, and 4.06 by :
Download or read book Aerodynamic Characteristics of a 60 Degree Sweptback-wing Airplane Configuration Having Tail Surfaces Located Outboard of the Wing Tips at Mach Numbers of 2.30, 2.97, 3.51, and 4.06 written by and published by . This book was released on 1960 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of a 60° Sweptback-wing Airplane Configuration Having Tail Surfaces Located Outboard of the Wingtips at Mach Numbers of 2.30, 2.97, 3.51, and 4.06 by : Sleeman, Jr. (William C.)
Download or read book Aerodynamic Characteristics of a 60° Sweptback-wing Airplane Configuration Having Tail Surfaces Located Outboard of the Wingtips at Mach Numbers of 2.30, 2.97, 3.51, and 4.06 written by Sleeman, Jr. (William C.) and published by . This book was released on 1960 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of a Wing with Quarter-chord Line Swept Back 60 Degrees, Aspect Ratio 2, Taper Ratio 0.6, and NACA 65A006 Airfoil Section by : Boyd C. Myers
Download or read book Aerodynamic Characteristics of a Wing with Quarter-chord Line Swept Back 60 Degrees, Aspect Ratio 2, Taper Ratio 0.6, and NACA 65A006 Airfoil Section written by Boyd C. Myers and published by . This book was released on 1950 with total page 31 pages. Available in PDF, EPUB and Kindle. Book excerpt: This paper presents the results of the investigation of a wing-alone and a wing-fuselage configuration employing a wing with quarter-chord line swept back 60 degrees, aspect ratio 2, taper ratio 0.6, and an NACA 65A006 airfoil section. The results are presented as lift, drag, pitching-moment and bending-moment coefficients for both configurations. In addition, effective downwash angles and point dynamic pressures for a range of tail heights at a probable tail length are presented for the two configurations investigated.
Book Synopsis The Subsonic Static Aerodynamic Characteristics of an Airplane Model Having a Triangular Wing of Aspect Ratio 3 by : Howard F. Savage
Download or read book The Subsonic Static Aerodynamic Characteristics of an Airplane Model Having a Triangular Wing of Aspect Ratio 3 written by Howard F. Savage and published by . This book was released on 1957 with total page 662 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been conducted to determine the effects of vertical-tail location and size on the subsonic aerodynamic characteristics of a model having a triangular wing. The wing had an aspect ratio of 3, an NACA 0003.5-63 section in the streamwise direction, and plain, trailing-edge ailerons. The wing was attached to the fuselage in either a mid or high position and an unswept horizontal tail was located on the fuselage center line. Two vertical tails were tested which had areas of 26.7 or 20.3 percent of the wing area. Each vertical tail was equipped with a rudder and had a geometric aspect ratio of 1.5, a taper ratio of 0.16, and 54 degrees of sweepback of the leading edge. Each vertical tail was tested at two different tail lengths. The wind-tunnel tests were conducted at a Reynolds number of 2.5 milMon at Mach numbers from 0.25 to 0.95.
Book Synopsis Aerodynamic Characteristics of Tapered Wings Having Aspect Ratios of 4, 6, and 8, Quarter-chord Lines Swept Back 45 Degrees, and NACA 63(sub 1)A012 Airfoil Sections by : Edward C. Polhamus
Download or read book Aerodynamic Characteristics of Tapered Wings Having Aspect Ratios of 4, 6, and 8, Quarter-chord Lines Swept Back 45 Degrees, and NACA 63(sub 1)A012 Airfoil Sections written by Edward C. Polhamus and published by . This book was released on 1951 with total page 23 pages. Available in PDF, EPUB and Kindle. Book excerpt: As part of a transonic research program conducted by the National Advisory Committee for Aeronautics, a series of wings is being investigated in the Langley high-speed 7- by 10-foot tunnel over a Mach number range of 0.70 to 1.15 by use of the transonic-bump technique.
Book Synopsis Aerodynamic Characteristics at Transonic Speeds of a Wing Having 45 Degrees Sweep, Aspect Ratio 8, Taper Ratio 0.45, and Airfoil Sections Varying from the NACA 63A010 Section at the Root to the NACA 63A006 Section at the Tip by : William D. Jr Morrison
Download or read book Aerodynamic Characteristics at Transonic Speeds of a Wing Having 45 Degrees Sweep, Aspect Ratio 8, Taper Ratio 0.45, and Airfoil Sections Varying from the NACA 63A010 Section at the Root to the NACA 63A006 Section at the Tip written by William D. Jr Morrison and published by . This book was released on 1952 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics at Supersonic Speeds of a Series of Wing-body Combinations Having Cambered Wings with an Aspect Ratio of 3.5 and a Taper Ratio of 0.2 by : Lowell E. Hasel
Download or read book Aerodynamic Characteristics at Supersonic Speeds of a Series of Wing-body Combinations Having Cambered Wings with an Aspect Ratio of 3.5 and a Taper Ratio of 0.2 written by Lowell E. Hasel and published by . This book was released on 1952 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
