Collection
Serial/Series Title
4 Matching Results
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Effects of vertical location of the wing and horizontal tail on the static lateral and directional stability of a trapezoidal-wing airplane model at Mach numbers of 1.41 and 2.01
Report presenting an investigation to determine the effects of vertical location of the wing and horizontal tail on the static lateral and directional stability at various combined angles of attack and sideslip for a supersonic airplane configuration at Mach numbers of 1.41 and 2.01. The configurations investigated included a high-wing, midwing, and low-wing arrangement in combination with horizontal-tail positions varying from a location of 0.208 wing semispan below to 0.556 semispan above the body center line.
Date:
July 9, 1958
Creator:
Robinson, Ross B.
System:
The UNT Digital Library
List of Reprints Available in the Technical Information Division
None
Date:
July 9, 1958
Creator:
unknown
System:
The UNT Digital Library
Panellit pressure effects with a loose front nozzle insert: K reactor I & E slugs
None
Date:
July 9, 1958
Creator:
Waters, E. D.
System:
The UNT Digital Library
Transonic Characteristics of Outboard Ailerons on a 4-Percent-Thick 30 Degree Sweptback Wing, Including Some Effects of Aileron Trailing-Edge Thickness and Aerodynamic Balance
Report presenting an investigation to determine the roll effectiveness, hinge-moment characteristics, and aileron center-of-load locations on an outboard 40-percent-semispan flap-type aileron on a 30 degree sweptback wing with an aspect ratio of 3.0, a taper ratio of 0.2, and NACA 65A004 airfoil sections. Results regarding general aileron characteristics and other aerodynamic characteristics are also presented.
Date:
July 9, 1958
Creator:
Whitcomb, Charles F. & Critzos, Chris C.
System:
The UNT Digital Library