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Friday, April 24, 2020 | History

3 edition of Wind-tunnel investigation of a full-scale canard-configured general aviation airplane found in the catalog.

Wind-tunnel investigation of a full-scale canard-configured general aviation airplane

Wind-tunnel investigation of a full-scale canard-configured general aviation airplane

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Published by National Aeronautics and Space Administration, Scientific and Technical Information Branch in [Washington, D.C.] .
Written in English

    Subjects:
  • Aerodynamic characteristics.,
  • Canard configurations.,
  • Control stability.,
  • Control surfaces.,
  • General aviation aircraft.,
  • Wind tunnel tests.

  • Edition Notes

    Other titlesWind tunnel investigation of a full scale canard-configured general aviation airplane.
    StatementLong P. Yip.
    SeriesNASA technical paper -- 2382.
    ContributionsUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL18218708M

    A General Aviation Technology Office was established within OAST in to develop the technology base for the design and development of safer, more productive, and superior U.S. general aviation aircraft. 10 NASA was responding to the growing importance of the general aviation segment of the U.S. civil air transportation system and the ever.


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Wind-tunnel investigation of a full-scale canard-configured general aviation airplane Download PDF EPUB FB2

A. ~ i 1 t 1 / I I' -1 I,Wind-Tunnel Investigation of the Flight Chasacteristics of a Canard Genera1:Aviation Airplane Coniiguration - I Dale R. Satran j. iNA3A N OE 7 - 1 d 0 3 j IHZ ELIGHT Cii G Fig32 AL- AVI A T [NASA) 60 p NASA) UIND- Ait ACiEiiI iUN AIRP TUNKEL.

Wind-Tunnel Investigation of a General Aviation Airplane Equipped With a High Aspect-Ratio, Natural-Laminar-Flow Wing An investigation has been conducted in the Langley by Foot Wind Tunnel to evaluate the performance and stability and control characteristics of a full-scale general aviation airplane equipped with a natural-laminar-flow by: 4.

As part of a broad research program to provide a data base on advanced airplane configurations, a wind-tunnel investigation was conducted in the Langley by Foot Wind Tunnel to determine the aerodynamic characteristics of an advanced canard-configured general aviation airplane.

The investigation included measurements of forces and moments Author: L. Yip and P. Coy. Full text of "Wind-tunnel investigation of a full-scale general aviation airplane equipped with an advanced natural laminar flow wing" See other formats NASA Technical Paper rWNSA National Aeronautics and Space Administration Scientific and Technical Information Division Wind-Tunnel Investigation of a Full- Scale General Aviation Airplane Equipped With an Advanced Natural.

Wind-tunnel investigation of a full-scale canard-configured general aviation airplane / By Long P. Yip and Langley Research Center. March "es bibliographical references (p. 10).Mode of Wind-tunnel investigation of a full-scale canard-configured general aviation airplane book Internet Topics: Airplanes.

Publisher: Washington, D.C.: National Aeronautics and Space Administration, Scientific and Technical Author: Long P.

Yip and Langley Research Center. Full-scale wind-tunnel investigation of the effects of wing leading-edge modifications on the high angle-of-attack aerodynamic characteristics of a low-wing general aviation airplane. JOHNSON, JR., W.

NEWSOM and D. SATRAN. Yip, L.P.: Wind-Tunnel Investigation of a Full Scale Canard-Configured General Aviation Airplane. NASA TP, March Wind-tunnel investigation of a full-scale canard-configured general aviation airplane book TP, March Google ScholarCited by: 6.

Tests were made in the Royal Aircraft Establishment No. 19 (18 in. x 18 in.) supersonic wind tunnel to measure the overall normal and side forces, rolling, pitching and Wind-tunnel investigation of a full-scale canard-configured general aviation airplane book moments on a typical canard aircraft layout Wind-tunnel investigation of a full-scale canard-configured general aviation airplane book M = and M = The complete configuration and configuration less fin,File Size: 5MB.

"Wind-tunnel tests on a 1/5-scale model of the Ryan XF2R airplane were conducted to determine the aerodynamic characteristics of the air intake for the front power plant, a General Electric TG gas turbine, and to determine the stability and control characteristics of the airplane.

The results indicated low-dynamic-pressure recovery for the air intake to the TG gas turbine with the Author: Park Y. Wong. A low speed wind tunnel test was conducted for a canard airplane model in KARI LSWT.

The purpose of the presented paper is to investigate the proper testing approach to correct tare precisely and. A Transonic Wind-Tunnel Investigation of a Seaplane Configuration Having a 40 Deg Sweptback Wing, Ted No. NACA de [Hieser, Gerald, Nasa Technical Reports Server (Ntrs), Et Al] on *FREE* shipping on qualifying offers.

A Transonic Wind-Tunnel Investigation of a Seaplane Configuration Having a 40 Deg Sweptback Wing, Ted No. NACA de Author: Gerald Hieser, Louis Kudlacik, W. Gray. Wind-tunnel investigation of a full-scale canard-configured general aviation airplane.

Washington, D.C.: National Aeronautics and Space Administration. Wind-tunnel investigation of a full-scale canard-configured general aviation airplane. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, Effects of wing-leading-edge modifications on a full-scale, low-wing general aviation airplane: Wind-tunnel investigation of high-angle-of-attack aerodynamic characteristics (NASA technical paper) [Newsom, William A] on *FREE* shipping on qualifying offers.

Effects of wing-leading-edge modifications on a full-scale, low-wing general aviation airplane: Wind-tunnel investigation of Author: William A Newsom. A full scale wind tunnel test was performed with a general aviation aircraft to investigate the use of the slipstream momentum survey method as a means of measuring propeller thrust in flight.

Aircraft angle of attack is shown to have significant influence on Author: S. Miley, Leonard S. Miller, Ken Hall, Houg-Jen Tsai.

Wind—Tunne1 Investigation of a Full—Scale and Coy, Paul F.: Yip, Long P. ; ICAS Paper No. August Canard—Configured General Aviation Aircraft. Richard White: Wind—Tunne1 Investigation of Effects of Wing Leading—Edge Modifications on the High Angle—of—Attack Characteristics of a T—Tai1 Low—Wing General File Size: 3MB.

Johnson, Joseph L., William A. Newsom, and Dale R. Satran Full-Scale Wind-Tunnel Investigation of the Effects of Wing Leading-Edge Modifications on the High Angle of Attack Aerodynamic Characteristics of a Low-Wing General Aviation Airplane, AIAA Paper Author: Malcolm J. Abzug, E.

Eugene Larrabee. An investigation was conducted in the Langley by Foot Tunnel to determine the aerodynamic characteristics of a powered, full-scale model of a general aviation airplane employing a canard.

A Look at Handling Qualities of Canard Configurations Seth B. Anderson CNASA-TM-StiJ54) ALeCK AT EAU)lING N The first human-powered flight was achieved by a canard-configured air­ designed and built without the benefit of wind tunnel tests, and documentationFile Size: 2MB.

rations roles, including aerodynamic data gathering in wind tunnel investigations for the analysis of full-scale. MODELING FLIGHT. aircraft designs, proof-of-concept demonstrators for radical aeronautical concepts, and problem-solving As a result of extensive correlation of results with subsequent full-scale.

YIP, L. Wind-tunnel investigation of a full-scale canard-configured general aviation airplane. NASA-TP Z. ZALOVCIK, JOHN A. Summary of stall-warning. "Wind-tunnel tests of a full-scale model of the Republic XP airplane were conducted to determine the longitudinal and lateral characteristics of the wing alone and the wing-fuselage combination, the characteristics of the aileron, and the damping in roll of the wing alone.

Various high-lift devices were investigated including trailing-edge split flaps and partial- and full-span leading-edge Author: Lynn W. Hunton, Joseph K. Dew. Full Scale Investigation of the Drag of a Wing Radiator.

Full Scale Tests of Wood Propellers on a VE-7 Airplane in the Propeller Research Tunnel. Full Scale Tests on a Thin Metal Propeller at Various Tip Speeds. Full-Scale Wind-Tunnel Tests of a Series of Metal Propellers on a VE-7 Airplane. Investigation of airframe and jet noise in high-speed flight with a microphone array.

Scaling and extrapolating small-scale in-flow wind tunnel jet noise to full-scale flyover jet noise. Christopher Allen, Paul Soderman, The noise from piston engine driven propellers on general aviation airplanes. Werner Dobrzynski, Burkhard Gehlhar.

A canard is an aeronautical arrangement wherein a small forewing or foreplane is placed forward of the main wing of a fixed-wing term "canard" may be used to describe the aircraft itself, the wing configuration, or the foreplane.

The term "canard" arose from the appearance of the Santos-Dumont bis ofwhich was said to be reminiscent of a duck (canard in French) with its.

Effects of Wing-Leading-Edge Modifications on a Full-Scale, Low-Wing General Aviation Airplane: Wind-Tunnel Investigation of High-Angle-of-Attack Aerodynamic Characteristics William A.

Newsom, Jr., Dale R. Satran, and Joseph L. Johnson, Jr. A selection has been made of NASA documents that will be useful for light and general aircraft.

We are providing these to our users as a useful reference source. These NASA documents have not been validated by ESDU but contribute to a comprehensive collection of design information and can be used along side ESDU methods for comparison and. Yip, "Wind-Tunnel Investigation of a Full-Scale Canard-Configured General Aviation Airplane," NASA TP, March "Ditching - Handbook for Pilots" -Frederick, MD: Aircraft Owners and Pilots Association,pp An investigation has been conducted in the Langley by Foot Wind Tunnel to evaluate the performance and stability and control characteristics of a full-scale general aviation airplane equipped with a natural-laminar-flow wing.

Historical. The earliest known examples of "push-pull" engined-layout aircraft include a trio of experimental German World War I designs: chronologically comprising the only Fokker twin-engined design of the period, the Fokker K.I from ; followed by the unusual Siemens-Schuckert DDr.I triplane fighter design of lateand concluding with the laterally-offset "push-pull" Gotha An investigation was conducted in the Langley by Foot Wind Tunnel to evaluate the performance, stability, and control characteristics of a full-scale general aviation airplane equipped with an advanced laminar flow wing.

The data obtained in the drag cleanup tests during World War II have been reissued in a modern report in order that they may be more available to the designers of modern general aviation aircraft. A full-size aircraft installed in the Langley full-scale tunnel for a drag cleanup investigation is shown in figure Aircraft 3; Bodies and Structures 2; Aircraft structures 2; Vehicle dynamics /flight dynamics 2; Tests and Testing 2; Canards 2; Flight tests 1; Business and general aviation aircraft 1; Wings 1; Entry, descent, and landing 1; Drag 1; Wind tunnel tests 1; Vertical take-off and landing (VTOL) 1; Center of gravity (CG) 1; Pitch 1; Stall 1.

In an aircraft with a pusher configuration (as opposed to a tractor configuration), the propeller(s) are mounted behind their respective engine(s). According to British aviation author Bill Gunston, a "pusher propeller" is one mounted behind the engine, so that the drive shaft is in compression.

Pusher configuration describes this specific (propeller or ducted fan) thrust device attached to a. Wind-Tunnel Data Correction Given that the purpose of wind tunnel testing is to predict the performance and behavior of a vehicle in flight, it is important to make corrections or adjustments to wind tunnel data to account for differences between the wind tunnel and flight environments.

These corrections generally fall into two Size: KB. Effects of wing-leading-edge modifications on a full-scale, low-wing general aviation airplane: wind-tunnel investigation of high-angle-of-attack aerodynamic characteristics / (Washington, D.C.: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va.

Icarus, rewaxed [microform]: a high speed, low-cost general aviation aircraft for "Aeroworld" / NASA/US Experimental study of noise transmission into a general aviation aircraft [microform] / R. Vaicaitis, D. Wind-tunnel investigation of a full-scale general aviation airplane equipped with an advanced natural la.

Fullscale wind tunnel investigation of the canard Rutan VariEze showed a propeller efficiency of compared to for a tractor configuration Canard-Configured airplanes, Philip W. Brown, Wind-Tunnel Investigation of a Full-Scale Canard-Configured General Aviation Airplane.

A wind-tunnel investigation of the first-order vibratory stresses on a full-scale supersonic-type propeller operating in an asymmetric air flow / (Washington, D.C.: National Advisory Committee for Aeronautics, ), by Atwood R.

Heath, Robert L. O'Neal, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for. International Journal of Aerospace Engineering / / Article.

Article Sections. Investigation of rain effect on aircraft flight was begun with the wind tunnel test, “Wind tunnel investigation of a full-scale canard-configured general aviation aircraft,” Tech.

Rep. TP, NASA, Cited by: 8. Search the catalogue for collection items held pdf the National Library of Australia. Book, Author: Murri, Frank, Description Wind-tunnel investigation of a full-scale general aviation airplane equipped with an advanced natural la.Photo, Print, Drawing An experimental scale model download pdf the B plane is prepared for wind tunnel tests in the plant of the North American Aviation, Inc., Inglewood, Calif.

The model maker holds an exact miniature reproduction of the type of bomb the plane will carry. This plant produces the battle-tested B bomber used in General Doolittle's raid on Tokyo, and the P ("Mustang") fighter.Engineering Science and ebook And his revolutionary Ag-1 and Piper Pawnee set ebook standards of lasting benefit to both the agricultural airplane and general aviation industries.

and brand new public facility was already paying off in spades by permitting a team of engineers to work in a wind tunnel with full-scale airplanes. Better.