Last edited by Vogore
Wednesday, May 13, 2020 | History

2 edition of Low-speed aerodynamic characteristics of a highly swept, untwisted, uncambered arrow wing found in the catalog.

Low-speed aerodynamic characteristics of a highly swept, untwisted, uncambered arrow wing

Paul L. Coe

Low-speed aerodynamic characteristics of a highly swept, untwisted, uncambered arrow wing

by Paul L. Coe

  • 242 Want to read
  • 22 Currently reading

Published by National Aeronautics and Space Administration, Scientific and Technical Information Branch, For the sale by the National Technical Information Service] in Washington, D.C, [Springfield, Va .
Written in English

    Subjects:
  • Airplanes -- Wings, Swept-back.,
  • Spoilers (Airplanes),
  • Aerodynamics, Supersonic.

  • Edition Notes

    StatementPaul L. Coe, Jr., Scott O. Kjelgaard, and Garl L. Gentry, Jr.
    SeriesNASA technical paper -- 2176.
    ContributionsKjelgaard, Scott O., Gentry, Garl L., United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
    The Physical Object
    Pagination67 p. :
    Number of Pages67
    ID Numbers
    Open LibraryOL17553419M

    For a subsonic airfoil, the aerodynamic center (the point of support) is approximately 25 percent of the way back from the wing leading edge. In supersonic flight, the aerodynamic center moves back to 50 percent of the wing’s chord, causing some significant changes in the airplane’s control and stability. Swept Wing and Sweep Angle Swept wings have a very low drag at high speed, and this is a bigger advantage than the disadvantages that swept wings have. The disadvantages are: Tip stalling. Pitching up at low speed stall. High angles of attack on approach at low speed results in high drag values. Top.

    To find if any aerodynamic advantages accrued from large streamwise edges, a model with a pure delta planform of aspect ratio was progressively cropped to give a series of models of lower aspect ratio, and the results of low-speed tunnel tests compared with. A supercritical airfoil is an airfoil designed primarily to delay the onset of wave drag in the transonic speed range. Supercritical airfoils are characterized by their flattened upper surface, highly cambered ("downward-curved") aft section, and larger leading-edge radius compared with NACA 6-series laminar airfoil shapes. Standard wing shapes are designed to create lower pressure over the.

    Airplanes -- Wings, Swept-back. See also what's at your library, or elsewhere. Broader terms: Airplanes; Airplanes -- Wings; Used for: Airplanes -- Wings, Oblique; Sweepback wings. In other words, high speed flow is associated with low pressure, and low speed flow with high pressure." (8) Since the air flowing above a wing is moving faster than that flowing beneath it, its pressure is less and an upward force is exerted on the wing. In his classic "Stick and Rudder" published more than sixty years ago, Wolfgang.


Share this book
You might also like
Viral Hepatitis B Infection in the Western Pacific Region

Viral Hepatitis B Infection in the Western Pacific Region

state in theory and practice.

state in theory and practice.

Living with less

Living with less

Interactions of silica wity iron oxides

Interactions of silica wity iron oxides

Public speaking made easy

Public speaking made easy

Stuck in a small world

Stuck in a small world

The Magician

The Magician

Ways of seeing/knowing

Ways of seeing/knowing

Ethical transformations for a sustainable future

Ethical transformations for a sustainable future

forgotten American

forgotten American

geometry of Rene Descartes

geometry of Rene Descartes

Discoveries in biological psychiatry.

Discoveries in biological psychiatry.

Radiation-induced rotation of small celestial bodies

Radiation-induced rotation of small celestial bodies

Low-speed aerodynamic characteristics of a highly swept, untwisted, uncambered arrow wing by Paul L. Coe Download PDF EPUB FB2

Low-speed aerodynamic characteristics of a highly swept, untwisted, uncambered arrow wing. Washington, D.C.: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. Low-speed aerodynamic characteristics of a highly swept arrow wing configuration with several deflected leading edge concepts by Gentry, G.

L., Jr.; Coe, P. L., Jr. I know there are advantages of swept-back wings delaying shock-wave allowing a aircraft to fly faster. However, what are the disadvantages. I know one of them is that they have very poor low speed characteristics, however I do not know the reason.

Low-speed aerodynamic characteristics of wings with sweep discontinuities. Authors; Authors and affiliations discontinuity is modelled by the introduction of a discontinuity in the equivalent vortex pattern chosen to replace the wing.

The total lift, induced drag, pitching moment coefficients and span-wise location of the centre of pressure Author: Sridhar M Ramachandra, Sheo Prakash. Air flowing over any swept wing tends to move spanwise towards the rearmost end of the wing.

On a rearward-swept wing this is outwards towards the tip, while on a forward-swept wing it is inwards towards the root. As a result, the dangerous tip stall condition of a rearward-swept design becomes a safer and more controllable root stall on a forward-swept design.

An investigation was conducted in the Langley 4- by 7-Meter Tunnel to provide a detailed study of wing pressure distributions and forces and moments acting on a highly swept arrow-wing model at. Look at the CL aircraft. This aircraft uncambered arrow wing book to fly slowly, because firefighting is more eficacious at low speeds.

Wikipedia: One rule is that such profiles usually have greater thicknesses, more camber (curvature of median line) for being bette. Forward-swept wing designs appear to offer selected aerodynamic performance improvements over conventional aft-swept wings, such as higher lift-drag ratios, lower trim drag, and better stall/spin characteristics (ref.

In addition, these designs may allow for. An investigation was conducted in a low-turbulence pressure tunnel to determine the two-dimensional lift and pitching-moment characteristics of an NACA and an NACA airfoil with percent-chord single-slotted flaps.

Both models were tested with flaps deflected from 0 deg to 45 deg, at angles of attack from minus 6 deg to several degrees past stall, at Reynolds numbers from Low-Speed Aerodynamics: From Wing Theory to Panel Methods | Free. low speed aerodynamic from wing theory panel methods (15 files+.

Low-Speed Aerodynamics: From Wing Theory to Panel Methods (Mcgraw-Hill Series in Aeronautical and Aerospace Engineering) by Joseph Katz, Allen Plotkin Low-Speed Aerodynamics: From Wing Theory to Panel Methods - pdf.

The X, the experimental forward swept wing aircraft designed by the NASA, was intended to validate studies that said forward swept wing should provide better control and lift qualities in extreme maneuvers, and possibly reduce aerodynamic drag as well as fly more efficiently at cruise speeds.

A numerical analysis is performed to investigate the aerodynamic characteristics and the static height stability of the endplate and the anhedral angle on an aspect-ratio-one wing-in-ground effect.

Jul 22,  · Aerodynamic characteristics at transonic speeds of a wing having a 45 degree sweep, aspect ratio 8, taper ratioand airfoil sections varying from the NACA 63A section at the root to the NACA 63A section at the innovationoptimiser.com: William D.

Morrison, Paul G. Fournier. Some studies have examined the aerodynamic characteristics of forward swept wing and prove number the identical transonic maneuver design conditions, a forward swept wing can be provide lesser drag than an equivalent aft swept wing [ 5,6 ].

For laminar flow wing, the reduction in sweep in the case of forward swept wing leads. A leading edge slot is a fixed aerodynamic feature of the wing of some aircraft to reduce the stall speed and promote good low-speed handling qualities. A leading edge slot is a spanwise gap in each wing, allowing air to flow from below the wing to its upper surface.

Oct 04,  · "An investigation has been conducted in the Langley MPH 7- by foot tunnel to determine the effect of negative dihedral, tip droop, and wing-tip shape on the low-speed aerodynamic characteristics of a complete model having a 45 degrees sweptback innovationoptimiser.com: M.

Leroy Spearman, Robert E. Becht. However, with the trailing-edge swept (arrow wing or cropped arrow wing), it has been found that the wing loadings in the vicinity of the trailing edge are highly sensitive to the trailing-edge sweep.

As a temporary fix to this problem, the near wake region has an additional boundary condition, AC = 0. An investigation was conducted in the Langley low turbulence pressure tunnel to determine the low-speed, two dimensional characteristics of a percent-thick supercritical airfoil.

The airfoil was tested at Reynolds numbers (based on chord) from million to million, at Mach numbers from toand at geometric angles of attack. This location is important in determining the aerodynamic characteristics of the airfoil. (4) The swept wing aircraft does not have an abrupt loss of lift at Cl(max).

Low speed stall will start at the wing's trailing edge. Where Cl/CL is a maximum. Pulling back on the control stick (or yoke) will cause the airplane to climb if the plane is. Note that unlike the aerodynamic center, the location of the center of pressure depends upon the lift coefficient.

Airfoil Drag Characteristics The drag on an airfoil (2-D wing) is primarily due to viscous effects at low speed and compressibility effects (wave drag) at. Apr 27,  · Yes of course. Wing produces two types of drag. (1) Parasite Drag (which is a combination of Form drag, Skin friction drag and Interference drag) (2) Induced Drag The total aerodynamic force generated by a wing is tilted backwards.

So it pro.An investigation was made to determine the effect of various high lift devices on a highly sweptforward wing with a leading edge sweep angle of 55 degrees and on a straight wing, both wings having an aspect ratio of and the same span. Experimental tests were made in the Cal Tech - Merrill low speed wind tunnel at Pasadena City College on both types of wing with and without innovationoptimiser.com: J.

E. Densmore.So we have to remove, from our calculations for each type of wing, the lift-induced drag, which had been greater in the straight wing. And this makes the straight wing drag coefficient lower at moderately high supersonic speeds, compared to the swept wing.