#
Airplanes -- Wings, Triangular
Resource Information
The concept ** Airplanes -- Wings, Triangular** represents the subject, aboutness, idea or notion of resources found in **University of Oklahoma Libraries**.

The Resource
Airplanes -- Wings, Triangular
Resource Information

The concept

**Airplanes -- Wings, Triangular**represents the subject, aboutness, idea or notion of resources found in**University of Oklahoma Libraries**.- Label
- Airplanes -- Wings, Triangular

- Authority link
- http://id.worldcat.org/fast/00803564

- Source
- fast

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- Wind-tunnel investigation of the aerodynamic characteristics in pitch and sideslip at high subsonic speeds of a wing-fuselage combination having a triangular wing of aspect ratio 4
- A note on the drag due to lift of delta wings at Mach numbers up to 2.0
- A preliminary wind-tunnel investigation of flutter characteristics of delta wings
- Aerodynamic characteristics of a delta wing with leading edge swept back 45 degrees, aspect ratio 4, and NACA 65A006 airfoil section : Transonic-bump method
- Aerodynamic characteristics of two delta wings and two trapezoidal wings at Mach number of 4.04
- Aerodynamic characteristics over a Mach number range of 1.40 to 2.78 of a rocket-propelled airplane configuration having a low 52.2° delta wing and an unswept horizontal tail
- Comparison of lift-curve slopes for a model tested in two slotted tunnels of different sizes at high subsonic speeds
- 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
- Damping in roll of cruciform and some related delta wings at supersonic speeds
- Damping in roll of models with 45°, 60°, and 70° delta wings determined at high subsonic, transonic, and supersonic speeds with rocket -powered models
- Dual methods and approximation concepts in structural synthesis
- Effect of some section modifications and protuberances on the zero-lift drag of delta wings at transonic and supersonic speeds
- 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
- Effects of size of external stores on the aerodynamic characteristics of an unswept and a 45° sweptback wing of aspect ratio 4 and a 60° delta wing at Mach numbers of 1.41, 1.62, and 1.96
- Effects of two leading-edge modifications on the aerodynamic characteristics of a thin low-aspect-ratio delta wing at transonic speeds
- Effects of wing position and fuselage size on the low-speed static and rolling stability characteristics of a delta-wing model
- Effects of wing position and vertical-tail configuration on stability and control characteristics of a jet-powered delta-wing vertically rising airplane model
- Experimental determination of damping in pitch of swept and delta wings at supersonic Mach numbers
- Experimental determination of the effects of frequency and amplitude of oscillation on the roll-stability derivatives for a 60° delta-wing airplane model
- Flutter of a 60° delta wing (NACA 65A003 airfoil) encountered at supersonic speeds during the flight test of a rocket-propelled model
- Investigation of the aerodynamic characteristics at high supersonic Mach numbers of a family of delta wings having double-wedge sections with the maximum thickness at 0.18 chord
- Investigations at supersonic speeds of 22 triangular wings representing two airfoil sections for each of 11 apex angles
- Lee-side flow over delta wings at supersonic speeds
- Lift and moment on oscillating triangular and related wings with supersonic edges
- Low-speed pitching derivatives of low-aspect-ratio wings of triangular and modified triangular plan forms
- Low-speed static lateral stability characteristics of a canard model having a 60° triangular wing and horizontal tail
- Low-speed static stability characteristics of a cambered-delta-wing model
- On the range of applicability of the transonic area rule
- Preliminary investigation at supersonic speeds of triangular and sweptback wings
- Some measurements at subsonic speeds of the aerodynamic forces and moments on two delta wings of aspect ratios 2 and 4 oscillating about the midchord
- Stability derivatives of triangular wings at supersonic speeds
- Supersonic flutter of a 60° delta wing encountered during the flight test of a rocket-propelled model
- The Calculation of downwash behind supersonic wings with an application to triangular plan forms
- The effects of fuselage size on the low-speed longitudinal aerodynamic characteristics of a thin 60° delta wing with and without a double slotted flap
- Three-dimensional unsteady lift problems in high-speed flight : the triangular wing
- Transonic flutter investigation of two 50° semispan modified-delta wings with tip ailerons
- Wind-tunnel investigation at high subsonic speeds to determine the rolling derivatives of two wing-fuselage combinations having triangular winds, including a semiempirical method of estimating the rolling derivatives
- Wind-tunnel investigation of damping in roll at supersonic speeds of triangular wings at angles of attack

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`<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.libraries.ou.edu/resource/jr7x8ELtPlU/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.libraries.ou.edu/resource/jr7x8ELtPlU/">Airplanes -- Wings, Triangular</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.libraries.ou.edu/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.libraries.ou.edu/">University of Oklahoma Libraries</a></span></span></span></span></div>`