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Effect Of Horizontal Tail Height On Aerodynamic Characteristics Of A Transport Model With A Variable Sweep Warped Wing
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Book Synopsis Effect of Horizontal-tail Height on Aerodynamic Characteristics of a Transport Model with a Variable-sweep Warped Wing by :
Download or read book Effect of Horizontal-tail Height on Aerodynamic Characteristics of a Transport Model with a Variable-sweep Warped Wing written by and published by . This book was released on 1965 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Aerodynamic Characteristics of a Tailless Fixed-wing Supersonic Transport Model by : Edward J. Ray
Download or read book Transonic Aerodynamic Characteristics of a Tailless Fixed-wing Supersonic Transport Model written by Edward J. Ray and published by . This book was released on 1966 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Memorandum written by and published by . This book was released on 1966 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1977 with total page 286 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Note written by and published by . This book was released on 1967 with total page 446 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Aerodynamic Characteristics of a Tailless Fixed-wing Supersonic Transport Model by : Edward J. Ray
Download or read book Transonic Aerodynamic Characteristics of a Tailless Fixed-wing Supersonic Transport Model written by Edward J. Ray and published by . This book was released on 1966 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Low-speed Aerodynamic Characteristics of a Transport Model Having 42.33 ̊swept Low Wing with Supercritical Airfoil, Double-slotted Flaps, and T-tail Or Low Tail by : Paul G. Fournier
Download or read book Low-speed Aerodynamic Characteristics of a Transport Model Having 42.33 ̊swept Low Wing with Supercritical Airfoil, Double-slotted Flaps, and T-tail Or Low Tail written by Paul G. Fournier and published by . This book was released on 1975 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :United States. National Aeronautics and Space Administration Scientific and Technical Information Division Publisher : ISBN 13 : Total Pages :428 pages Book Rating :4.F/5 ( download)
Book Synopsis NASA Scientific and Technical Reports by : United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Download or read book NASA Scientific and Technical Reports written by United States. National Aeronautics and Space Administration Scientific and Technical Information Division and published by . This book was released on 1968 with total page 428 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Wing Pivot Location on Longitudinal Aerodynamic Characteristics of a Variable Sweep Wing Having an M Planform by :
Download or read book Effect of Wing Pivot Location on Longitudinal Aerodynamic Characteristics of a Variable Sweep Wing Having an M Planform written by and published by . This book was released on 1964 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Longitudinal Aerodynamic Effects of Sweeping Up the Rear of the Fuselage of a Rocket-propelled Airplane Model Having No Horizontal Tail by : James H. Parks
Download or read book Transonic Longitudinal Aerodynamic Effects of Sweeping Up the Rear of the Fuselage of a Rocket-propelled Airplane Model Having No Horizontal Tail written by James H. Parks and published by . This book was released on 1955 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Some Effects of Tail Height and Wing Plan Form on the Static Longitudinal Stability Characteristics of a Small-scale Model at High Subsonic Speeds by : Albert G. Few
Download or read book Some Effects of Tail Height and Wing Plan Form on the Static Longitudinal Stability Characteristics of a Small-scale Model at High Subsonic Speeds written by Albert G. Few and published by . This book was released on 1954 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt: The drag due to lift increases with increasing sweep through the Mach number range. Some increase in bag due to lift is evident decrease in taper ratio for wings having 300of sweep through most of the speed range.
Author :United States. National Aeronautics and Space Administration. Scientific and Technical Information Division Publisher : ISBN 13 : Total Pages :436 pages Book Rating :4.E/5 ( download)
Book Synopsis A Selected Listing of NASA Scientific and Technical Reports by : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Download or read book A Selected Listing of NASA Scientific and Technical Reports written by United States. National Aeronautics and Space Administration. Scientific and Technical Information Division and published by . This book was released on 1968 with total page 436 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Low-speed Aerodynamic Characteristics of a Supersonic Transport Model with a High-aspect-ratio Variable-sweep Warped Wing by :
Download or read book Low-speed Aerodynamic Characteristics of a Supersonic Transport Model with a High-aspect-ratio Variable-sweep Warped Wing written by and published by . This book was released on 1964 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Longitudinal Aerodynamic Characteristics of a Variable-sweep Fighter Model Having Body-mounted Nacelles by :
Download or read book Transonic Longitudinal Aerodynamic Characteristics of a Variable-sweep Fighter Model Having Body-mounted Nacelles written by and published by . This book was released on 1964 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental and Theoretical Investigation at High Subsonic Speeds of the Effects of Horizontal-tail Height on the Aerodynamic Characteristics in Sideslip of an Unswept, Untapered Tail Assembly by : Harleth G. Wiley
Download or read book An Experimental and Theoretical Investigation at High Subsonic Speeds of the Effects of Horizontal-tail Height on the Aerodynamic Characteristics in Sideslip of an Unswept, Untapered Tail Assembly written by Harleth G. Wiley and published by . This book was released on 1953 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Horizontal-tail Height and a Wing Leading-edge Modification Consisting of a Full-span Flap and a Partial-span Chord-extension on the Aerodynamic Characteristics in Pitch at High Subsonic Speeds of a Model with a 45 Degree Sweptback Wing by : William D. Jr Morrison
Download or read book Effects of Horizontal-tail Height and a Wing Leading-edge Modification Consisting of a Full-span Flap and a Partial-span Chord-extension on the Aerodynamic Characteristics in Pitch at High Subsonic Speeds of a Model with a 45 Degree Sweptback Wing written by William D. Jr Morrison and published by . This book was released on 1953 with total page 37 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Investigation of Aerodynamic Characteristics of a Swept-wing Fighter-airplane Model with Leading-edge Droop in Combination with Outboard Chord-extensions and Notches by : Charles F. Whitcomb
Download or read book Transonic Investigation of Aerodynamic Characteristics of a Swept-wing Fighter-airplane Model with Leading-edge Droop in Combination with Outboard Chord-extensions and Notches written by Charles F. Whitcomb and published by . This book was released on 1956 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation of the effects of several wing leading-edge modifications on the aerodynamic characteristics of a 45 degree swept-wing fighter-airplane model has been conducted in the Langley 16-foot transonic tunnel at low and high lifting conditions at Mach numbers from 0.85 to 1.03. The investigation included the determination of the effect on longitudinal stability and performance characteristics of wing leading-edge and chord-extension droops of 6 and 20 degrees, chord-extension overhangs of 0.075c and 0.15c (where c is the wing chord), leading-edge notches cut out at the inboard end of the 0.075c chord-extension to depths of 0.075c and 0.125c, and indentation of the model fuselage to conform partially to the supersonic area rule for a Mach number of 1.20. Lift, drag, and pitching-moment data were obtained for configurations with the tail on and off. Comparisons of data obtained from the present model with data from a configuration with leading-edge slats are included.
