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Book Low speed Aerodynamic Characteristics of a Wing canard Configuration with Underwing Spanwise Blowing on the Trailing edge Flap System

Download or read book Low speed Aerodynamic Characteristics of a Wing canard Configuration with Underwing Spanwise Blowing on the Trailing edge Flap System written by Daniel W. Banks and published by . This book was released on 1987 with total page 126 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Low speed Aerodynamic Characteristics of a Wing canard Configuration with Underwing Spanwise Blowing on the Trailing edge Flap System

Download or read book Low speed Aerodynamic Characteristics of a Wing canard Configuration with Underwing Spanwise Blowing on the Trailing edge Flap System written by Daniel W. Banks and published by . This book was released on 1987 with total page 118 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Low speed Longitudinal Characteristics of an Airplane Configuration Including Effects of Canard and Wing Trailing edge Flap Controls in Combination

Download or read book Low speed Longitudinal Characteristics of an Airplane Configuration Including Effects of Canard and Wing Trailing edge Flap Controls in Combination written by Bernard Spencer and published by . This book was released on 1962 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book NASA Technical Memorandum

Download or read book NASA Technical Memorandum written by and published by . This book was released on 1987 with total page 668 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Scientific and Technical Aerospace Reports

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1987 with total page 1126 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

Book Monthly Catalogue  United States Public Documents

Download or read book Monthly Catalogue United States Public Documents written by and published by . This book was released on 1995-11 with total page 944 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book NASA Technical Paper

Download or read book NASA Technical Paper written by and published by . This book was released on 1988 with total page 146 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Low speed Investigation of Effects of Wing Leading  and Trailing edge Flap Deflections and Canard Incidence on a Fighter Configuration Equipped with a Forward swept Wing

Download or read book Low speed Investigation of Effects of Wing Leading and Trailing edge Flap Deflections and Canard Incidence on a Fighter Configuration Equipped with a Forward swept Wing written by Thomas G. Gainer and published by . This book was released on 1984 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Low speed Aerodynamic Characteristics of a Canard Airplane Configuration Having Split Flaps Located Ahead of the Wing Trailing Edge and Leading and Trailing edge Flaps on the Canard Control

Download or read book Low speed Aerodynamic Characteristics of a Canard Airplane Configuration Having Split Flaps Located Ahead of the Wing Trailing Edge and Leading and Trailing edge Flaps on the Canard Control written by BERNARD JR. SPENCER and published by . This book was released on 1962 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: The investigation was conducted at low subsonic speeds in the Langley 300-MPH 7- by 10-foot tunnel. The basic wing was trapezoidal in planform with an aspect ratio of 3.0, a taper ratio of 0.143, and a leading-edge sweep of 38.52 degrees. Modifications to the basic wing included deflectable partial-span leading-edge chord-extensions, plain lift flaps located at the trailing edge, and split flaps located forward of the trailing edge. A trapezoidal canard surface similar in planform to the wing, a 60 degrees delta surface and a modified 60 degree delta canard suface were tested in conjunction with the wing. Use of trailing-edge flaps located on the 60 degrees delta and trapezoidal canard surfaces was also investigated as possible longitudinal controls. (Author).

Book NASA SP

    Book Details:
  • Author :
  • Publisher :
  • Release : 1988
  • ISBN :
  • Pages : 520 pages

Download or read book NASA SP written by and published by . This book was released on 1988 with total page 520 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Effects of Canard Planform and Wing leading edge Modification on Low speed Longitudinal Aerodynamic Characteristics of a Canard Airplane Configuration

Download or read book Effects of Canard Planform and Wing leading edge Modification on Low speed Longitudinal Aerodynamic Characteristics of a Canard Airplane Configuration written by Bernard Spencer and published by . This book was released on 1961 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been conducted at low subsonic speeds to study the effects of canard planform and wing-leading-edge modification on the longitudinal aerodynamic characteristics of a general research canard airplane configuration. The basic wing of the model had a trapezoidal planform, an aspect ratio of 3.0, a taper ratio of 0.143, and an unswept 80-percent-chord line. Modifications to the wing included addition of full-span and partial-span leading-edge chord-extensions. Two canard planforms were employed in the study one was a 60° sweptback delta planform and the other was a trapezoidal planform similar to that of the basic wing. Modifications to these canards included addition of a full-span leading-edge chord-extension to the trapezoidal planform and a fence to the delta planform. For the basic-wing-trapezoidal-canard configuration, rather abrupt increases in stability occurred at about 12° angle of attack. A slight pitch-up tendency occurred for the delta-canard configuration at approximately 8° angle of attack. A comparison of the longitudinal control effectiveness for the basic-wing-trapezoidal-canard combination and for the basic-wing-delta-canard combination indicates higher values of control effectiveness at low angles of attack for the trapezoidal canard. The control effectiveness for the delta-canard configuration, however, is seen to hold up for higher canard deflections and to higher angles of attack. Use of a full-span chord-extension deflected approximately 30° on the trapezoidal canard greatly improved the control characteristics of this configuration and enabled a sizeable increase in trim lift to be realized.

Book Aeronautical Engineering

Download or read book Aeronautical Engineering written by and published by . This book was released on 1988 with total page 518 pages. Available in PDF, EPUB and Kindle. Book excerpt: A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA).

Book Monthly Catalog of United States Government Publications  Cumulative Index

Download or read book Monthly Catalog of United States Government Publications Cumulative Index written by United States. Superintendent of Documents and published by . This book was released on 1976 with total page 1466 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Aeronautical Engineering  A Cumulative Index to a Continuing Bibliography

Download or read book Aeronautical Engineering A Cumulative Index to a Continuing Bibliography written by and published by . This book was released on 1988 with total page 516 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Aerodynamics in Ground Effect and Predicted Landing Ground Roll of a Fighter Configuration with a Secondary nozzle Thrust Reverser

Download or read book Aerodynamics in Ground Effect and Predicted Landing Ground Roll of a Fighter Configuration with a Secondary nozzle Thrust Reverser written by Daniel W. Banks and published by . This book was released on 1988 with total page 136 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Low speed Longitudinal Characteristics of Airplane Configuration Including Effects of Canard and Wing Trailing edge Flap Controls in Combination  with List of References

Download or read book Low speed Longitudinal Characteristics of Airplane Configuration Including Effects of Canard and Wing Trailing edge Flap Controls in Combination with List of References written by and published by . This book was released on 1959 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt: