Aerodynamic Characteristics Of A 60 Degree Sweptback Wing Airplane Configuration Having Tail Surfaces Located Outboard Of The Wing Tips At Mach Numbers Of 230 297 351 And 406 PDF Download
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| Author | : Sleeman, Jr. (William C.) |
| Publisher | : |
| Total Pages | : 56 |
| Release | : 1960 |
| Genre | : Aerodynamic measurements |
| ISBN | : |
Download 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 Book in PDF, ePub and Kindle
| Author | : |
| Publisher | : |
| Total Pages | : 54 |
| Release | : 1960 |
| Genre | : |
| ISBN | : |
Download 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 Book in PDF, ePub and Kindle
| Author | : Sleeman, Jr. (William C.) |
| Publisher | : |
| Total Pages | : 49 |
| Release | : 1960 |
| Genre | : Aerodynamic measurements |
| ISBN | : |
Download 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 Book in PDF, ePub and Kindle
| Author | : James D. Church |
| Publisher | : |
| Total Pages | : 48 |
| Release | : 1958 |
| Genre | : |
| ISBN | : |
Download Investigation of Aerodynamic Characteristics of an Airplane Configuration Having Tail Surfaces Outboard of the Wing Tips at Mach Numbers of 2.30, 2.97, and 3.51 Book in PDF, ePub and Kindle
| Author | : M. Leroy Spearman |
| Publisher | : |
| Total Pages | : 34 |
| Release | : 1957 |
| Genre | : Airplanes |
| ISBN | : |
Download Investigation of the Aerodynamic Characteristics in Pitch and Sideslip of a 45© Swept-wing Airplane Configuration with Various Vertical Locations of the Wing and Horizontal Tail Book in PDF, ePub and Kindle
An investigation has been conducted in the Langley 4- by 4-foot supersonic pressure tunnel to determine the effects of wing and horizontal-tail vertical location on the aerodynamic characteristics in sideslip at various angles of attack for a supersonic airplane configuration at Mach numbers of 1.41 and 2.01. The basic model was equipped with a wing and horizontal tail, each having 45 degree sweep and an aspect ratio of 4. The wing had a taper ratio of 0.2 and NACA 65A004 sections; the horizontal tail had a taper ratio of 0.4 and NACA 65A006 sections.
| Author | : Gerald V. Foster |
| Publisher | : |
| Total Pages | : 32 |
| Release | : 1960 |
| Genre | : Aerodynamics |
| ISBN | : |
Download Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2.20 of a Variable-wing-sweep STOL Configuration Book in PDF, ePub and Kindle
| Author | : |
| Publisher | : |
| Total Pages | : 28 |
| Release | : 1960 |
| Genre | : |
| ISBN | : |
Download Aerodynamic Characteristics in Pitch at a Mach Number of 1.97 of Two Variable-wing- Sweep V/STOL Configurations with Outboard Wing Panels Swept Back 75 Deg Book in PDF, ePub and Kindle
| Author | : Emma Jean Landrum |
| Publisher | : |
| Total Pages | : 40 |
| Release | : 1962 |
| Genre | : Airplanes |
| ISBN | : |
Download A Tabulation of Section Aerodynamic Characteristics at Mach Numbers of 1.61 and 2.01 for Four Swept Wings Having the Same Planform But Different Surface Shapes Book in PDF, ePub and Kindle
| Author | : Gerald V. Foster |
| Publisher | : |
| Total Pages | : 38 |
| Release | : 1960 |
| Genre | : Aerodynamics, Supersonic |
| ISBN | : |
Download Stability and Control Characteristics at Mach Numbers of 2.50, 3.00, and 3.71 of a Variable- Wing-sweep Configuration with Outboard Wing Panels Swept Back 75° Book in PDF, ePub and Kindle
| Author | : Odell A. Morris |
| Publisher | : |
| Total Pages | : 32 |
| Release | : 1961 |
| Genre | : Airplanes |
| ISBN | : |
Download 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 Book in PDF, ePub and Kindle
