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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
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**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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- 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 comparison of the experimental aerodynamic characteristics of an oblique wing with those of a swept wing
- 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 swept wing panel in a low speed flexible walled test section
- 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
- A transonic interactive boundary-layer theory for laminar and turbulent flow over swept wings
- AGARD standard aeroelastic configurations for dynamic response : candidate configuration I.-wing 445.6
- ALESEP, Part II : a computer program for the analysis of leading edge separation bubbles on infinite swept wings
- 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 derivatives for an oblique wing aircraft estimated from flight data by using a maximum likelihood technique
- 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
- Aerodynamics of slender wings and wing-body combinations having swept trailing edges
- Air forces and moments on triangular and related wings with subsonic leading edges oscillating in supersonic potential flow
- 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
- Analysis of iced wings
- Approximate corrections for the effects of compressibility on the subsonic stability derivatives of swept wings
- Assessment of potential aerodynamic benefits from spanwise blowing at the wingtip
- Boundary layer relaminarization device : patent application
- Charts for determining the pitching moment of tapered wings with sweepback and twist
- 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
- Crossflow stability and transition experiments in a swept-wing flow
- Damping-in-pitch characteristics at high subsonic and transonic speeds of four 35° sweptback wings
- Downstream influence of swept slot injection in hypersonic turbulent flow
- 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
- Dual methods and approximation concepts in structural synthesis
- Effect of Kruger nose flaps on the experimental force and moment characteristics of an oblique wing
- 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 drooped-nose flaps on the experimental force and moment characteristics of an oblique wing
- 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 leading-edge radius and Reynolds number on longitudinal aerodynamic characteristics of highly swept wing-body configurations at subsonic speeds
- 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
- Flight-measured buffet characteristics of a supercritical wing and a conventional wing on a variable-sweep airplane
- 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°
- High performance forward swept wing aircraft : patent application
- In-flight total forces, moments, and static aeroelestic characteristics of an oblique-wing research airplane
- 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
- Lift-curve slopes determined in flight on a flexible swept-wing jet bomber
- 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 aerodynamic characteristics of a highly swept, untwisted, uncambered arrow wing
- 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
- Nonlinear wave interactions in swept wing flows
- Note on the relative effect of the dihedral and the sweep back of airplane wings
- Numerical simulation of swept-wing flows : a progress report for graduate program in aeronautics
- On the stability of an infinite swept attachment line boundary layer
- Preliminary investigation at low speeds of swept wings in rolling flow
- Pressure distributions induced by elevon deflections on swept wings and adjacent end-plate surfaces at Mach 6
- 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
- Status of linear boundary-layer stability theory and the en method, with emphasis on swept-wing applications
- Supersonic flutter of a 60° delta wing encountered during the flight test of a rocket-propelled model
- Swept wing attachment line contamination fence
- Tests with three-dimensional adjustments in the rectangular working section of the French T2 wind tunnel, with an AS 07-type swept-back wing model
- The aerodynamic behavior of a harmonically oscillating finite sweptback wing in supersonic flow
- 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
- The rolling moment due to sideslip of swept wings at subsonic and transonic speeds
- The twisting effect at transonic speeds of spoiler ailerons on a 45° sweptback, aspect-ratio-4, tapered wing
- Theoretical and experimental investigation of ground-induced effects for a low-aspect-ratio highly swept arrow-wing configuration
- 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
- Validation of a pair of computer codes for estimation and optimization of subsonic aerodynamic performance of simple hinged-flap systems for thin swept wings
- Wind tunnel pressure distribution tests on a series of biplane wing models, Part II, Effects of changes in decalage, dihedral, sweepback and overhang
- Wind tunnel pressure distribution tests on a series of biplane wing models, Part III :, Effects of changes in various combinations of stagger, gap, sweepback and decalage
- 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 at low speed of the effect of varying the ratio of body diameter to wing span from 0.1 to 0.8 on the aerodynamic characteristics in pitch of the 45° sweptback-wing--body combination
- 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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