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Effects Of Vertical Location Of Wing And Horizontal Tail On The Aerodynamic Characteristics In Pitch At Mach Numbers From 060 To 140 Of An Airplane Configuration With An Unswept Wing
Download Effects Of Vertical Location Of Wing And Horizontal Tail On The Aerodynamic Characteristics In Pitch At Mach Numbers From 060 To 140 Of An Airplane Configuration With An Unswept Wing full books in PDF, epub, and Kindle. Read online Effects Of Vertical Location Of Wing And Horizontal Tail On The Aerodynamic Characteristics In Pitch At Mach Numbers From 060 To 140 Of An Airplane Configuration With An Unswept Wing ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Book Synopsis Effects of Vertical Location of Wing and Horizontal Tail on the Aerodynamic Characteristics in Pitch at Mach Numbers from 0.60 to 1.40 of an Airplane Configuration with an Unswept Wing by : Louis S. Stivers
Download or read book Effects of Vertical Location of Wing and Horizontal Tail on the Aerodynamic Characteristics in Pitch at Mach Numbers from 0.60 to 1.40 of an Airplane Configuration with an Unswept Wing written by Louis S. Stivers and published by . This book was released on 1957 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation was conducted to determine the effects of vertical location of an unswept wing and horizontal tail on the aerodynamic characteristics in pitch of a wing-body-tail combination. The wing had an aspect ratio of 3.09, a taper ratio of 0.39, and quarter-chord line swept back 11.5 degrees, and biconvex sections. Lift, drag, and pitching-moment coefficients were obtained at Mach numbers from 0.60 to 1.40 for angles of attack from -4 to approximately 13 degrees, with the boundary-layer transition on the model fixed and free. The Reynolds number of the tests was 1.5 million, based on the wing mean aerodynamic chord. The effects of Mach number on the experimental and calculated lift curve slopes, pitching-moment curve slopes, and contributions of the horizontal tail to the pitching-moment curve slopes are presented for the various wing and horizontal-tail locations.
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:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781725184299 Total Pages :34 pages Book Rating :4.1/5 (842 download)
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 : National Aeronautics and Space Administration (NASA)
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 National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-08-13 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: Experimental investigations have been conducted to determine the effect of wing vertical position and horizontal-tail vertical and axial position on the static aerodynamic characteristics of a wing-body horizontal-tail configuration. The configurations investigated included the wing in a high, mid, or low position on the body with the horizontal tail in each of these vertical positions as well as in three axial positions. The closest position of the horizontal tail to the wing essentially provided on all-wing configuration. In addition, tests were made for the three wing positions with the horizontal tail removed. The tests were made in three different wind tunnels to provide data for a Mach number range from 0.25 to 4.63. The purpose of the investigation was to illustrate the strong effects of interference flow fields as a function of geometry and flight regime. An analysis of the results indicate some arrangements that might lead to aerodynamic problems and others in which the interference flow fields might be favorably exploited. The results suggest that a coplanar concept with a translating horizontal tail could potentially minimize the aerodynamic changes with Mach number and provide more optimum performance over the Mach number range. Spearman, M. L. Langley Research Center NASA-TM-84643, NAS 1.15:84643 RTOP 505-43-43-01...
Book Synopsis Investigation of the Aerodynamic Characteristics in Pitch and Sideslip of a 45 Degree Swept-wing Airplane Configuration with Various Vertical Locations of the Wing and Horizontal Tail by : M. Leroy Spearman
Download or read book Investigation of the Aerodynamic Characteristics in Pitch and Sideslip of a 45 Degree Swept-wing Airplane Configuration with Various Vertical Locations of the Wing and Horizontal Tail written by M. Leroy Spearman and published by . This book was released on 1957 with total page 29 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Wing Planform on the Aerodynamic Characteristics of a Wing-body-tail Model at Mach Numbers 1.57, 2.16, and 2.87 by : Royce L. McKinney
Download or read book Effects of Wing Planform on the Aerodynamic Characteristics of a Wing-body-tail Model at Mach Numbers 1.57, 2.16, and 2.87 written by Royce L. McKinney and published by . This book was released on 1965 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Wing Planform on the Aerodynamic Characteristics of a Wing-body-tail Model at Mach Numbers 3.96 and 4.63 by : Maurice O. Feryn
Download or read book Effects of Wing Planform on the Aerodynamic Characteristics of a Wing-body-tail Model at Mach Numbers 3.96 and 4.63 written by Maurice O. Feryn and published by . This book was released on 1966 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Wing Height on the Stability and Control Characteristics at a Mach Number of 2.01 of a Canard Airplane Configuration with a 70° Delta Wing by : Cornelius Driver
Download or read book Effects of Wing Height on the Stability and Control Characteristics at a Mach Number of 2.01 of a Canard Airplane Configuration with a 70° Delta Wing written by Cornelius Driver and published by . This book was released on 1960 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Lateral Characteristics at High Subsonic Speeds of a Complete Airplane Model with a Highly Tapered Wing Having the 0.80 Chord Line Unswept and with Several Tail Configuration by : Kenneth W. Goodson
Download or read book Static Lateral Characteristics at High Subsonic Speeds of a Complete Airplane Model with a Highly Tapered Wing Having the 0.80 Chord Line Unswept and with Several Tail Configuration written by Kenneth W. Goodson and published by . This book was released on 1961 with total page 102 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was made at high subsonic speeds of a complete model having a highly tapered wing and several tail configurations. The aspect-ratio-3.50 wing had a taper of 0.067 and an unswept 0.80 chord line. The complete model was tested with a wing-chord-plane tail, a T-tail, and a biplane tail (combined T-tail and wing-chord-plane tail). The model was tested in the Langley high-speed 7- by 10-foot tunnel at Mach numbers from 0.60 to 0.92 over a range of angle of attack of about ±20° and a range of sideslip of -15° to 13°. Some data were obtained with the horizontal stabilizer deflected. A few tests were also made with the wing tips clipped to an aspect ratio of 3.00.
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 Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2.01 of a Tailless Delta V/STOL Configuration Having Variable-sweep Wing Panels by : M. Leroy Spearman
Download or read book Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2.01 of a Tailless Delta V/STOL Configuration Having Variable-sweep Wing Panels written by M. Leroy Spearman and published by . This book was released on 1961 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Horizontal-tail Span and Vertical Location on the Aerodynamic Characteristics of an Unswept Tail Assembly in Sideslip by : Donald R. Riley
Download or read book Effect of Horizontal-tail Span and Vertical Location on the Aerodynamic Characteristics of an Unswept Tail Assembly in Sideslip written by Donald R. Riley and published by . This book was released on 1953 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been conducted in the Langley stability tunnel on a vertical-tail model with a stub fuselage in combination with various horizontal tails to determine the effect of horizontal-tail span and vertical location of the horizontal tail relative to the vertical tail on the aerodynamic characteristics of an unswept tail assembly in sideslip.
Book Synopsis Effect of Wing Pivot Location on Longitudinal Aerodynamic Characteristics of a Variable-sweep Wing Having an M Planform by : William P. Henderson
Download or read book Effect of Wing Pivot Location on Longitudinal Aerodynamic Characteristics of a Variable-sweep Wing Having an M Planform written by William P. Henderson and published by . This book was released on 1964 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Wing Vertical Location on the Stability and Control Characteristics at a Mach Number of 2.01 of a Canard Airplane Configuration with a Trapezoidal Aspect-ratio-3 Wing by : Gerald V. Foster
Download or read book Effects of Wing Vertical Location on the Stability and Control Characteristics at a Mach Number of 2.01 of a Canard Airplane Configuration with a Trapezoidal Aspect-ratio-3 Wing written by Gerald V. Foster and published by . This book was released on 1959 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of Aerodynamic Characteristics in Pitch and Sideslip of a 45 Degree Sweptback-wing Airplane Model with Various Vertical Locations of Wing and Horizontal Tail by : M. Leroy Spearman
Download or read book Investigation of Aerodynamic Characteristics in Pitch and Sideslip of a 45 Degree Sweptback-wing Airplane Model with Various Vertical Locations of Wing and Horizontal Tail written by M. Leroy Spearman and published by . This book was released on 1956 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been conducted in the Langley 4- by 4-foot supersonic pressure tunnel to determine the effects of various vertical locations of the wing and horizontal tail on the aerodynamic characteristics in pitch of a supersonic airplane configuration at a Mach number of 2.01. The model is equipped with a wing and horizontal tail, each having a 45 degree sweep and an aspect ratio of 4. The wing had a taper ratio of 0.2 with NACA 65A004 airfoil sections, whereas the horizontal tail had a taper ratio of 0.6 with NACA 65A006 airfoil sections.
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 Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2.20 of a V/STOL Airplane Configuration with a Variable-sweep Wing and with a Skewed Wing Design by :
Download or read book Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2.20 of a V/STOL Airplane Configuration with a Variable-sweep Wing and with a Skewed Wing Design written by and published by . This book was released on 1961 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
