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Airplanes -- Wings, Swept-back
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The concept ** Airplanes -- Wings, Swept-back** represents the subject, aboutness, idea or notion of resources found in **University of Oklahoma Libraries**.

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Airplanes -- Wings, Swept-back
Resource Information

The concept

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

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- http://id.worldcat.org/fast/00803560

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- fast

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- Wind-tunnel investigation of the effects of steady rolling on the aerodynamic loading characteristics of a 45° sweptback wing at high subsonic speeds
- A Comparison of the lateral controllability with flap and plug ailerons on a sweptback-wing model having full-span flaps
- A Simple method of estimating the subsonic lift and damping in roll of sweptback wings
- A buffet investigation at high subsonic speeds of wing-fuselage-tail combinations having sweptback wings with NACA 64A thickness distributions, fences, a leading-edge extension, and body contouring
- A comparison at mach numbers up to 0.92 of the calculated and experimental downwash and wake characteristics at various horizonatl tail heights behind a wing with 45 degrees of sweepback
- A flight investigation of the transonic area rule for a 52.5° sweptback wind-body configuration at Mach numbers between 0.8 and 1.6
- A study of the use of experimental stability derivatives in the calculation of the lateral disturbed motions of a swept-wing airplane and comparison with flight results
- A tabulation of wind-tunnel pressure data at Mach numbers of 1.61 and 2.01 of five swept wings of the same plan form but different surface shapes
- Aerodynamic characteristics at supersonic speeds of a series of wing-body combinations having cambered wings with an aspect ratio of 3.5 and a taper ratio of 0.2 : effect at M = 1.60 of nacelle shape and position on the aerodynamic characteristics in pitch of two wing-body combinations with a 47° sweptback 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 a leading-edge slat on a 35 degree swept-back wing for Mach numbers from 0.30 to 0.88
- Aerodynamic load measurements and opening characteristics of automatic leading-edge slats on a 45° sweptback wing at transonic speeds
- Aerodynamic loading characteristics in sideslip of a 45° sweptback wing with and without a fence at high subsonic speeds
- Airplane motions and loads induced by flying through the flow field generated by an airplane at low supersonic speeds
- An analysis of the effects of aeroelasticity on static longitudinal stability and control of a swept-back-wing airplane
- An experimental study of a method of designing the sweptback-wing - fuselage juncture for reducing the drag at transonic speeds
- An experimental transonic investigation of a 45° sweptback wing-body combination with several types of body indentation with theoretical comparisons included
- An investigation at transonic speeds of the effects of thickness ratio and of thickened root sections on the aerodynamic characteristics of wings with 47° sweepback, aspect ratio 3.5, and taper ratio 0.2 in the slotted test section of the Langley 8-foot high-speed tunnel
- An investigation of a supersonic aircraft configuration having a tapered wing with circular-arc sections and a 40° sweepback : pressure distribution measurements of the interference effect of the wing on the fuselage at Mach numbers of 1.40 and 1.59
- An investigation of the effects of a geometric twist on the aerodynamic loading characteristics of a 45° sweptback wing-body configuration at transonic speeds
- An investigation of the hydrodynamic characteristics of a dynamic model of a transonic seaplane design having a planing-tail hull
- Approximate corrections for the effects of compressibility on the subsonic stability derivatives of swept wings
- Comparison of semispan data obtained in the Langley two-dimensional low-turbulence pressure tunnel and full-span data obtained in the Langley 19-foot pressure tunnel for a wing with a 40° sweepback of the 0.27-chord line
- Damping-in-pitch characteristics at high subsonic and transonic speeds of four 35° sweptback wings
- Downwash characteristics and vortex-sheet shape behind a 63 degree swept-back wing-fuselage combination at a Reynolds number of 6,100,000
- Dual methods and approximation concepts in structural synthesis
- Effect of airfoil profile of symmetrical sections on the low-speed rolling derivatives of 45° sweptback-wing models of aspect ratio 2.61
- Effect of aspect ratio and sweepback on the low-speed lateral control characteristics of untapered low-aspect-ratio wings equipped with retractable ailerons
- Effect of horizontal-tail location on low-speed static longitudinal stability and damping in pitch of a model having 45° sweptback wing and tail surfaces
- Effect of horizontal-tail size and tail length on low-speed static longitudinal stability and damping in pitch of a model having 45° sweptback wing and tail surfaces
- Effect of longitudinal wings position on the pressure characteristics at transonic speeds of a 45° sweptback wing-fuselage model
- Effects of a sweptback hydrofoil on the force and longitudinal stability characteristics of a typical high-speed airplane
- 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 twist and camber on the low-speed longitudinal stability characteristics of a 45° swept-back wing of aspect ratio 8 at Reynolds numbers from 1.5 x 106 to 4.8 x 10 as determined by pressure distributions, force tests, and calculations
- Effects of wing-tip droop on the longitudinal characteristics of two highly swept wing-body combinations at Mach numbers from 0.6 to 1.4
- Experimental aerodynamic forces and moments at low speed of a missile model during simulated launching from the midsemispan location of a 45 degree sweptback wing-fuselage combination
- Experimental and analytical investigation of flutter of a nonuniform sweptback cantilever wing with two concentrated weights
- Experimental and predicted longitudinal response characteristics of a large flexible 35 degree swept-wing airplane at an altitude of 35,000 feet
- Experimental determination of damping in pitch of swept and delta wings at supersonic Mach numbers
- Experimental determination of effect of structural rigidity on rolling effectiveness of some straight and swept wings at Mach numbers from 0.7 to 1.7
- Flight calibration of four airspeed systems on a swept-wing airplane at Mach numbers up to 1.04 by the NACA radar-phototheodolite method
- Flight tests of a leading-edge area suction on a fighter-type airplane with a 35 degree sweptback wing
- Flutter characteristics of swept wings at transonic speeds
- Flutter investigation at low speed of a 40 degree sweptback wing with pylon-mounted stores, tested as a semispan-cantilever wing and as a full-span wing on a towed airplane model
- Flutter investigation of two thin, low-aspect-ratio, swept, solid, metal wings in the transonic range by use of free-falling body
- Flutter of a 60° delta wing (NACA 65A003 airfoil) encountered at supersonic speeds during the flight test of a rocket-propelled model
- General theory of wave-drag reduction for combinations employing quasi-cylindrical bodies with an application to swept-wing and body combinations
- Gust-tunnel investigation of a flexible-wing model with semichord line line swept back 45°
- Influence of large amounts of wing sweep on stability and control problems of aircraft
- Investigation at Mach numbers from 0.80 to 1.43 of pressure and load distributions over a thin 45° sweptback highly tapered wing in combination with basic and indented bodies
- Investigation at transonic speeds of the loading over a 45 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2, and NACA 65A004 airfoil sections
- 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 : Static lateral and directional stability ; Mach numbers of 1.41 and 2.01
- Investigation of the effects of leading-edge chord-extensions and fences in combination with leading-edge flaps on the aerodynamic characteristics at Mach numbers of 0.40 to 0.93 of a 45° sweptback wing of aspect ratio 4
- Investigation of three tapered 45° sweptback cambered and twisted wings covering a simultaneous variation in aspect ratio and thickness ratio and of one related symmetrical wing at transonic speeds by the wing-flow method
- Investigation of transonic flutter characteristics of a thin 10 degree sweptback wing having an aspect ratio of 4 and a taper ratio of 0.6
- Investigation of wing flutter at transonic speeds for six systematically varied wing plan forms
- Lateral-control investigation of flap-type controls on a wing with quarter-chord line sweptback 35°, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil section : Transonic-bump method
- Leading-edge deflection optimization for a highly swept arrow-wing configuration
- Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds : plane 45° swept-back wing of aspect ratio 3, taper ratio 0.4 with 3-percent-thick, biconvex section
- Linearized lifting-surface theory for swept-back wings with slender plan forms
- Longitudinal stability and trim of two rocket-propelled airplane models having 45° sweptback wings and tails with the horizontal tail mounted in two positions
- Longitudinal stability characteristics at transonic speeds of a rocket-propelled model of an airplane having a 45 degree swept wing of aspect ratio 6.0
- Low-speed wind-tunnel investigation of a triangular sweptback air inlet in the root of a 45 degree sweptback wing
- Low-speed wind-tunnel investigation of jet control on a 35° swept wing
- Measurements of fluctuating pressures on the wing of a sweptback wind-body combination in the Langley 16-foot transonic tunnel
- Preliminary investigation at low speeds of swept wings in rolling flow
- Rolling and yawing moments for swept-back wings in sideslip at supersonic sppeds
- Some low-speed wind-tunnel experiments pertaining to the longitudinal stability characteristics of a 35° swept-wing model and an unswept-wing model
- Span loadings due to wing twist at transonic and supersonic speeds
- Supersonic flutter of a 60° delta wing encountered during the flight test of a rocket-propelled model
- The calculation of span load distributions on swept-back wings
- The effects of mass distribution on the low-speed dynamic lateral stability and control characteristics of a model with a 45° sweptback wing
- The effects of wing incidence on the aerodynamic loading characteristics of a sweptback wing-body combination at transonic speeds
- Theoretical lift and damping in roll of thin sweptback wings of arbitrary taper and sweep at supersonic speeds : Subsonic leading edges and trailing edges
- Theoretical loading at supersonic speeds of flat swept-back wings with interacting trailing and leading edges
- Transonic flight tests to compare the zero-lift drag on underslung and symmetrical nacelles varied chordwise at 40 percent semispan of a 45° sweptback, tapered wing
- Transonic flight tests to determine the effect of thickness ratio and plan-form modification on the zero-lift drag of a 45° sweptback wing
- Transonic investigation at lifting conditions of streamline contouring in the sweptback-wing-fuselage juncture in combination with the transonic area rule
- Transonic investigation of aerodynamic characteristics of a swept-wing fighter-airplane model with leading-edge droop in combination with outboard chord-extensions and notches
- Transonic wind-tunnel investigation of the effects of aspect ratio, spanwise variations in section thickness ratio, and a body indentation on the aerodynamic characteristics of a 45° sweptback wing-body combination
- Transonic wind-tunnel investigation of the effects of sweepback and thickness ratio on the wing loads of a wing-body combination of aspect ratio 4 and taper ratio 0.6
- Transonic wind-tunnel investigation of the interference between a 45° sweptback wing and a systematic series of four bodies
- Wind-tunnel investigation at high subsonic speeds of the effect of spoiler profile on the lateral control characteristics of a wing-fuselage combination winter quarter-chord line swept back 32.6° and NACA 65A006 airfoil section
- Wind-tunnel investigation of effect of sweep on rolling derivatives at angles of attack up to 13° and at high subsonic Mach numbers, including a semiempirical method of estimating the rolling derivatives
- 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

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