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Book Wind Tunnel Tests at High Subsonic Speeds on a Half model of the Prototype Handley Page  Victor  B 35 46 Wing and Fuselage

Download or read book Wind Tunnel Tests at High Subsonic Speeds on a Half model of the Prototype Handley Page Victor B 35 46 Wing and Fuselage written by J. R. Collingbourne and published by . This book was released on 1953 with total page 21 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Technical Report

    Book Details:
  • Author : Aeronautical Research Council (Great Britain)
  • Publisher :
  • Release : 1967
  • ISBN :
  • Pages : 872 pages

Download or read book Technical Report written by Aeronautical Research Council (Great Britain) and published by . This book was released on 1967 with total page 872 pages. Available in PDF, EPUB and Kindle. Book excerpt: Includes its Reports, which are also issued separately.

Book Reports and Memoranda

Download or read book Reports and Memoranda written by and published by . This book was released on 1961 with total page 864 pages. Available in PDF, EPUB and Kindle. Book excerpt: Beginning with no. 650 each hundredth number contains a list of the Reports and memoranda published since the last list.

Book Wind tunnel Investigation at High Subsonic Speeds of Some Effects of Fuselage Cross section Shape and Wing Height on the Static Longitudinal and Lateral Stability Characterisitcs of a Model Having a 45 Degree Swept Wing

Download or read book Wind tunnel Investigation at High Subsonic Speeds of Some Effects of Fuselage Cross section Shape and Wing Height on the Static Longitudinal and Lateral Stability Characterisitcs of a Model Having a 45 Degree Swept Wing written by Thomas J. Jr King and published by . This book was released on 1956 with total page 61 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Wind Tunnel Flutter Tests at Subsonic Speeds on an Half Wing with a Fan Engine

Download or read book Wind Tunnel Flutter Tests at Subsonic Speeds on an Half Wing with a Fan Engine written by D. A. Drane and published by . This book was released on 1976 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Wind Tunnel Tests of Fuselages and Windscreens

Download or read book Wind Tunnel Tests of Fuselages and Windscreens written by Edward Pearson Warner and published by . This book was released on 1925 with total page 552 pages. Available in PDF, EPUB and Kindle. Book excerpt: The tests described herein were made in 1918, in the old four-foot wind tunnel at the Massachusetts Institute of Technology and at the request of the Engineering Division of the U.S. Army Air Service.

Book A Wind tunnel Investigation at Subsonic and Low Supersonic Speeds of a Re entry Vehicle with Retractable Wings

Download or read book A Wind tunnel Investigation at Subsonic and Low Supersonic Speeds of a Re entry Vehicle with Retractable Wings written by Willard G. Smith and published by . This book was released on 1961 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Low speed Wind tunnel Tests on a Wing fuselage Model with Area Suction Through Perforations at the Leading edge Flap Knee

Download or read book Low speed Wind tunnel Tests on a Wing fuselage Model with Area Suction Through Perforations at the Leading edge Flap Knee written by S. F. J. Butler and published by . This book was released on 1967 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book High speed Wind tunnel Tests of a Twin fuselage Pursuit Airplane

Download or read book High speed Wind tunnel Tests of a Twin fuselage Pursuit Airplane written by Joseph L. Anderson and published by . This book was released on 1946 with total page 120 pages. Available in PDF, EPUB and Kindle. Book excerpt: At the request of the Air Technical Service Command, U. S. Army Air Forces, a 0.22-scale model of a twin-fuselage pursuit airplane was built and tested at the Ames Aeronautical Laboratory. The tests of this model were made in order that the aerodynamic characteristics of the airplane, especially at high speed, might be predicted.

Book Wind tunnel Investigation at High Subsonic Speeds of the Effects of Wing mounted External Stores on the Loading and Aerodynamic Characteristics in Pitch of a 45 Degree Sweptback Wing Combined with a Fuselage

Download or read book Wind tunnel Investigation at High Subsonic Speeds of the Effects of Wing mounted External Stores on the Loading and Aerodynamic Characteristics in Pitch of a 45 Degree Sweptback Wing Combined with a Fuselage written by H. Norman Silvers and published by . This book was released on 1954 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Full Scale Subsonic Wind Tunnel Requirements and Design Studies

Download or read book Full Scale Subsonic Wind Tunnel Requirements and Design Studies written by Mark W. Kelly and published by . This book was released on 1972 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Wind tunnel Investigation at High Subsonic Speeds of the Static Longitudinal and Static Lateral Stability Characteristics of a Wing fuselage Combination Having a Triangular Wing of Aspect Ratio 2 31 and an NACA 65A003 Airfoil

Download or read book Wind tunnel Investigation at High Subsonic Speeds of the Static Longitudinal and Static Lateral Stability Characteristics of a Wing fuselage Combination Having a Triangular Wing of Aspect Ratio 2 31 and an NACA 65A003 Airfoil written by James W. Wiggins and published by . This book was released on 1953 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book High speed Wind tunnel Tests of Gun Openings in the Nose of the Fuselage of a 1 4 scale Model

Download or read book High speed Wind tunnel Tests of Gun Openings in the Nose of the Fuselage of a 1 4 scale Model written by Henry A. Fedziuk and published by . This book was released on 1942 with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt: In connection with recent tests of a 1/4-scale model pursuit airplane in the NACA 8-foot high-speed tunnel, gun openings have low drag were developed for installation in the nose of the fuselage. The increase in the fuselage-drag coefficient for the final form of the openings was 0.0132 at a Mach number of 0.69 and at an angle of attack of zero degrees. The corresponding drag coefficient based on the wing area was about 0.0005. The critical speed of the airplane was not affected by the gun openings.