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Investigation Of The Effects Of Body Camber And Body Indentation On The Longitudinal Characteristics Of A 60 Degree Delta Wing Body Combination At A Mach Number Of 161
Download Investigation Of The Effects Of Body Camber And Body Indentation On The Longitudinal Characteristics Of A 60 Degree Delta Wing Body Combination At A Mach Number Of 161 full books in PDF, epub, and Kindle. Read online Investigation Of The Effects Of Body Camber And Body Indentation On The Longitudinal Characteristics Of A 60 Degree Delta Wing Body Combination At A Mach Number Of 161 ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Book Synopsis Investigation of the Effects of Body Camber and Body Indentation on the Longitudinal Characteristics of a 60 Degree Delta-wing-body Combination at a Mach Number of 1.61 by : John R. Sevier
Download or read book Investigation of the Effects of Body Camber and Body Indentation on the Longitudinal Characteristics of a 60 Degree Delta-wing-body Combination at a Mach Number of 1.61 written by John R. Sevier and published by . This book was released on 1956 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been made in the Langley 4- by 4-foot supersonic pressure tunnel to determine the effects of body camber and body indentation on the longitudinal characteristics of a delta-wing-body combination at a Mach number of 1.61. In combination with a 3-percent-thick 60 degree delta wing, the following three bodies were tested: (1) a basic parabolic body (Sears-Haack), (2) a body indented so as to have an improved wing-body area distribution at a Mach number of 1.8, and (3) a body which was both indented and cambered.
Book Synopsis Investigation of the Effects of Body Indentation and of Wing-plan-form Modification on the Longitudinal Characteristics of a 60 Degree Swept-wing Body Combination at Mach Numbers of 1.41, 1.61, and 2.01 by : John R. Jr Sevier
Download or read book Investigation of the Effects of Body Indentation and of Wing-plan-form Modification on the Longitudinal Characteristics of a 60 Degree Swept-wing Body Combination at Mach Numbers of 1.41, 1.61, and 2.01 written by John R. Jr Sevier and published by . This book was released on 1955 with total page 37 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Wing Incidence on the Longitudinal Trim Characteristics of a Cambered 70 Deg Delta-wing Configuration at Mach Numbers 3.0 to 5.0 by :
Download or read book Effects of Wing Incidence on the Longitudinal Trim Characteristics of a Cambered 70 Deg Delta-wing Configuration at Mach Numbers 3.0 to 5.0 written by and published by . This book was released on 1960 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Investigation at a Mach Number of 2.01 of the Effects of Body Cross-section Shape on the Aerodynamic Characteristics of Bodies and Wing-body Combinations by : Harry W. Carlson
Download or read book An Experimental Investigation at a Mach Number of 2.01 of the Effects of Body Cross-section Shape on the Aerodynamic Characteristics of Bodies and Wing-body Combinations written by Harry W. Carlson and published by . This book was released on 1955 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: Abstract: An experimental investigation has been performed to determine the effect of changes in body cross-section shape on the aerodynamic characteristics of bodies and wing-body combinations. A series of 13 bodies having a given length and given longitudinal distribution of cross-sectional area but various cross-section shapes were tested at a Mach number of 2.01. The bodies were tested alone and in combination with a 47° sweptback wing having a 6-percent-thick hexagonal section.
Book Synopsis An Investigation of the Influence of Body Size and Indentation Asymmetry on the Effectiveness of Body Indentation in Combination with a Cambered Wing by : James C. Patterson
Download or read book An Investigation of the Influence of Body Size and Indentation Asymmetry on the Effectiveness of Body Indentation in Combination with a Cambered Wing written by James C. Patterson and published by . This book was released on 1961 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Transonic Wind-tunnel Investigation of the Effects of Twist and Camber with and Without Incidence, Twist, and Body Indentation on the Aerodynamic Characteristics of a 45 Degree Sweptback Wing-body Configuration by : J. Lawrence Cooper
Download or read book A Transonic Wind-tunnel Investigation of the Effects of Twist and Camber with and Without Incidence, Twist, and Body Indentation on the Aerodynamic Characteristics of a 45 Degree Sweptback Wing-body Configuration written by J. Lawrence Cooper and published by . This book was released on 1954 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Wing Section and Body Vertical Location on the Longitudinal Aerodynamic Characteristics at Mach Number 4.63 of a Configuration Having a 70 Deg Delta Wing and a Low Volume Body by :
Download or read book Effects of Wing Section and Body Vertical Location on the Longitudinal Aerodynamic Characteristics at Mach Number 4.63 of a Configuration Having a 70 Deg Delta Wing and a Low Volume Body written by and published by . This book was released on 1961 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Body Indentation on the Drag Characteristics of a Delta-wing-body Combination at Transonic Speeds by : Dewey E. Wornom
Download or read book Effects of Body Indentation on the Drag Characteristics of a Delta-wing-body Combination at Transonic Speeds written by Dewey E. Wornom and published by . This book was released on 1955 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Subsonic Investigation of Effects of Body Indentation on Zero-lift Drag Characteristics of a 45 Degree Sweptback Wing-body Combination with Natural and Fixed Boundary-layer Transition Through a Range of Reynolds Number 1 X (10)6 to 8 X (10)6 by : Gene J. Bingham
Download or read book Subsonic Investigation of Effects of Body Indentation on Zero-lift Drag Characteristics of a 45 Degree Sweptback Wing-body Combination with Natural and Fixed Boundary-layer Transition Through a Range of Reynolds Number 1 X (10)6 to 8 X (10)6 written by Gene J. Bingham and published by . This book was released on 1954 with total page 10 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Low-speed Performance and Static Longitudinal Stability and Control Characteristics of a 60 Degree-delta-wing-body-tail Combination with Blowing Over Trailing-edge Flaps by : William I. Scallion
Download or read book Investigation of the Low-speed Performance and Static Longitudinal Stability and Control Characteristics of a 60 Degree-delta-wing-body-tail Combination with Blowing Over Trailing-edge Flaps written by William I. Scallion and published by . This book was released on 1957 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Aerodynamic Characteristics of a Wing-Body Combination Having a 52.5 Deg Sweptback Wing of Aspect Ratio 3 with Conical Camber and Designed for a Mach Number of the Square Root of 2 by : William B. Igoe
Download or read book Transonic Aerodynamic Characteristics of a Wing-Body Combination Having a 52.5 Deg Sweptback Wing of Aspect Ratio 3 with Conical Camber and Designed for a Mach Number of the Square Root of 2 written by William B. Igoe and published by . This book was released on 1961 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Transonic Wind-tunnel Investigation of the Effects of Body Indentation on the Aerodynamic Characteristics of an Approximate-delta-wing-body Configuration, and a Comparison with a Wing of Reversed Plan Form by : Claude V. Williams
Download or read book A Transonic Wind-tunnel Investigation of the Effects of Body Indentation on the Aerodynamic Characteristics of an Approximate-delta-wing-body Configuration, and a Comparison with a Wing of Reversed Plan Form written by Claude V. Williams and published by . This book was released on 1953 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Body Camber on Aerodynamic Characteristics of a Lifting Entry Vehicle Model at Mach Numbers from 2.30 to 4.62 by :
Download or read book Effects of Body Camber on Aerodynamic Characteristics of a Lifting Entry Vehicle Model at Mach Numbers from 2.30 to 4.62 written by and published by . This book was released on 1966 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of an All-movable Wing-tip Control on the Longitudinal Stability of 60 Degree Sweptback-wing-indented-body Configuration Equipped with Fences at Transonic Speeds by : Thomas L. Fischetti
Download or read book Effect of an All-movable Wing-tip Control on the Longitudinal Stability of 60 Degree Sweptback-wing-indented-body Configuration Equipped with Fences at Transonic Speeds written by Thomas L. Fischetti and published by . This book was released on 1955 with total page 15 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been made to obtain the effects of a 20-percent-semispan all-movable wing-tip control (which was deflected -5 to -10 degrees) on the longitudinal stability characteristics of a twisted and cambered 60 degrees sweptback-wing-indented-body configuration equipped with fences at angles of attack which generally varied from 0 to 16 degrees and over the Mach number range of 0.80 to 1.13. The Reynolds number based on the mean aerodynamic chord varied from 2,010,000 to 2,220,000.
Book Synopsis The Effect of Conical Camber on the Static Longitudinal, Lateral, and Directional Characteristics of a 45-degree Sweptback Wing at Mach Numbers Up to 0.96 by : Robert I. Sammonds
Download or read book The Effect of Conical Camber on the Static Longitudinal, Lateral, and Directional Characteristics of a 45-degree Sweptback Wing at Mach Numbers Up to 0.96 written by Robert I. Sammonds and published by . This book was released on 1956 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been conducted to determine the effect of conical camber on the drag due to lift and on the static longitudinal, lateral, and directional stability characteristics of an aspect-ratio-3, 45 degree sweptback wing in combination with a streamline body. Tests were made at Mach numbers up to 0.96 at a Reynolds number of 1.5 million and at a Reynolds number up to 8 million at a Mach number of 0.22, both with and without roughness strips near the leading edge of both the upper and lower surfaces of the wing.
Book Synopsis A Transonic Investigation of Changing Indentation Design Mach Number on the Aerodynamic Characteristics of a 45 Degrees Sweptback-wing-body Combination Designed for High Performance by : Donald L. Loving
Download or read book A Transonic Investigation of Changing Indentation Design Mach Number on the Aerodynamic Characteristics of a 45 Degrees Sweptback-wing-body Combination Designed for High Performance written by Donald L. Loving and published by . This book was released on 1956 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt:
