Effects Of An Inset Tab On The Hinge Moment And Effectiveness Characteristics Of An Unswept Trailing Edge Control On A 60c Delta Wing At Mach Numbers From 075 To 196
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Author | : Lawrence D. Guy |
Publisher | : |
Total Pages | : 35 |
Release | : 1955 |
Genre | : |
ISBN | : |
Download Effects of an Inset Tab on the Hinge-moment and Effectiveness Characteristics of an Unswept Trailing-edge Control on a 60 Degree Delta Wing at Mach Numbers from 0.75 to 1.96 Book in PDF, Epub and Kindle
Author | : Lawrence Duncan Guy |
Publisher | : |
Total Pages | : 42 |
Release | : 1955 |
Genre | : Airplanes |
ISBN | : |
Download Effects of an Inset Tab on the Hinge-moment and Effectiveness Characteristics of an Unswept Trailing-edge Control on a 60© Delta Wing at Mach Numbers from 0.75 to 1.96 Book in PDF, Epub and Kindle
Author | : Odell A. Morris |
Publisher | : |
Total Pages | : 36 |
Release | : 1955 |
Genre | : |
ISBN | : |
Download Effects of a Detached Tab on the Hinge-moment and Effectiveness Characteristics of an Unswept Trailing-edge Control on a 60 Degree Delta Wing at Mach Numbers from 0.75 to 1.96 Book in PDF, Epub and Kindle
Author | : Lawrence D. Guy |
Publisher | : |
Total Pages | : 52 |
Release | : 1954 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
Download Effects of Overhang Balance on the Hinge-moment and Effectiveness Characteristics of an Unswept Trailing-edge Control on a 60 Degree Delta Wing at Transonic and Supersonic Speeds Book in PDF, Epub and Kindle
A wind-tunnel investigation has been made of two unswept, partial-span, flap-type controls (differing only in hinge-line location) mounted on a 60 degree delta wing. One control was unbalanced and the other has a 100-percent overhang balance. Control hinge moments as well as aerodynamic characteristics of the complete wing-body combination were obtained for control deflections from 0 to 40 degrees over an angle-of-attack range of plus or minus 12 degrees at Mach numbers from 0.75 to 1.96. Reynolds numbers varied between 2,200,000 and 2,200,000. Expressions derived from linear theory for the hinge-moment coefficient due to angle of attack for unswept partial-span controls (which extend neither to the wing tip nor to the wing center line) on triangular wings having subsonic leading edges are given in an appendix.
Author | : Odell A. Morris |
Publisher | : |
Total Pages | : 38 |
Release | : 1953 |
Genre | : Airplanes |
ISBN | : |
Download Control Hinge-movement and Effectiveness Characteristics of Several Interchangeable Tip Controls on a 60© Delta Wing at Mach Numbers of 1.41, 1.62, and 1.96 Book in PDF, Epub and Kindle
Author | : Lawrence Duncan Guy |
Publisher | : |
Total Pages | : 154 |
Release | : 1956 |
Genre | : Aerofoils |
ISBN | : |
Download Investigation of the Effects of Inset and Detached Tabs on the Hinge-moment and Effectiveness Characteristics of an Unswept Trailingedge Control on a 60 D̊elta Wing at Transonic and Supersonic Mach Numbers Book in PDF, Epub and Kindle
Author | : Lawrence D. Guy |
Publisher | : |
Total Pages | : 53 |
Release | : 1957 |
Genre | : |
ISBN | : |
Download Hinge-moment and Effectiveness Characteristics of an Aspect-ratio-8.2 Flap-type Control on a 60 Degrees Delta Wing at Mach Numbers from 0.72 to 1.96 Book in PDF, Epub and Kindle
Author | : K.R. Czarnecki |
Publisher | : |
Total Pages | : 43 |
Release | : 1953 |
Genre | : |
ISBN | : |
Download Preliminary Investigation of the Effect of Fences and Balancing Tabs on the Hinge-moment Characteristics of a Tip Control on a 60 Degree Delta Wing at Mach Number 1.61 Book in PDF, Epub and Kindle
Author | : Odell A. Morris |
Publisher | : |
Total Pages | : 33 |
Release | : 1953 |
Genre | : |
ISBN | : |
Download Control Hinge-moment and Effectiveness Characteristics of Several Interchangeable Tip Controls on a 60 Degree Delta Wing at Mach Numbers of 1.41, 1.62. and 1.96 Book in PDF, Epub and Kindle
Author | : Lawrence D. Guy |
Publisher | : |
Total Pages | : |
Release | : 1953 |
Genre | : |
ISBN | : |
Download Control Hinge-moment and Effectiveness Characteristics of a 60 Degrees Half-delta Tip Control on a 60 Degrees Delta Wing at Mach Numbers of 1.41 and 1.96 Book in PDF, Epub and Kindle