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Book Pressure distribution Measurements of Two Airfoil Models with Fowler Flaps Submitted by Consolidated Aircraft Corporation as Alternative Wing Sections of the XB 32 Airplane

Download or read book Pressure distribution Measurements of Two Airfoil Models with Fowler Flaps Submitted by Consolidated Aircraft Corporation as Alternative Wing Sections of the XB 32 Airplane written by Ira H. Abbott and published by . This book was released on 1942 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: Pressure-distribution measurements were made on two 24-inch chord models equipped with Fowler flaps and submitted by the Consolidated Aircraft Corporation. The tests were made in the Langley two-dimensional low-turbulence pressure tunnel.

Book Wartime Report

    Book Details:
  • Author : United States. National Advisory Committee for Aeronautics
  • Publisher :
  • Release :
  • ISBN :
  • Pages : 296 pages

Download or read book Wartime Report written by United States. National Advisory Committee for Aeronautics and published by . This book was released on with total page 296 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Wartime Report

Download or read book Wartime Report written by and published by . This book was released on 1944 with total page 734 pages. Available in PDF, EPUB and Kindle. Book excerpt: Reproductions of reports, some declassified, of research done at Langley Memorial Aeronautical Laboratory during World War II. The order of reports does not represent when they were chronologically issued. Reference to the original version of each report is included.

Book NACA Wartime Report

    Book Details:
  • Author : United States. National Advisory Committee for Aeronautics
  • Publisher :
  • Release : 1942
  • ISBN :
  • Pages : 578 pages

Download or read book NACA Wartime Report written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1942 with total page 578 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Technical Note   National Advisory Committee for Aeronautics

Download or read book Technical Note National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1957 with total page 472 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Index of NACA Technical Publications

Download or read book Index of NACA Technical Publications written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1947 with total page 448 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Effects of Thermal Relaxation and Specific heat Changes on Measurements with a Pneumatic probe Pyrometer

Download or read book Effects of Thermal Relaxation and Specific heat Changes on Measurements with a Pneumatic probe Pyrometer written by P. W. Kuhns and published by . This book was released on 1957 with total page 736 pages. Available in PDF, EPUB and Kindle. Book excerpt: Equations are derived to evaluate the effects of thermal vibration relaxation and specific-heat changes on pneumatic-probe pyrometer measurements in the region 1000 to 3000 degrees K and 0.3

Book Catalogue of Publications Issued by the Government of the United States

Download or read book Catalogue of Publications Issued by the Government of the United States written by United States. Superintendent of Documents and published by . This book was released on 1948 with total page 1334 pages. Available in PDF, EPUB and Kindle. Book excerpt: February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index

Book Pressure distribution Measurements of a Model of a Davis Wing Section with Fowler Flap Submitted by Consolidated Aircraft Corporation

Download or read book Pressure distribution Measurements of a Model of a Davis Wing Section with Fowler Flap Submitted by Consolidated Aircraft Corporation written by Ira H. Abbott and published by . This book was released on 1942 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt: Wing pressure distribution diagrams for several angles of attack and flap deflections of 0 degrees, 20 degrees, and 40 degrees are presented. The normal force coefficients agree with lift coefficients obtained in previous test of the same model, except for the maximum lifts with flap deflection. Pressure distribution measurements were made at Reynolds Number of about 6,000,000.

Book NASA Contractor Report

Download or read book NASA Contractor Report written by and published by . This book was released on 1969 with total page 1366 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Technical Information Pilot

Download or read book Technical Information Pilot written by and published by . This book was released on 1948 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Monthly catalog of the United States government publications

Download or read book Monthly catalog of the United States government publications written by and published by . This book was released on 1948 with total page 1794 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Pressure distribution Measurements of a Low drag Airfoil with Slotted Flap Submitted by Curtiss Wright Corporation

Download or read book Pressure distribution Measurements of a Low drag Airfoil with Slotted Flap Submitted by Curtiss Wright Corporation written by Ira H. Abbott and published by . This book was released on 1941 with total page 10 pages. Available in PDF, EPUB and Kindle. Book excerpt: Pressure-distribution measurements were made on a 24-inch-chord wooden model equipped with a slotted flap and submitted by the Curtiss-Wright Corporation. The tests were made in the Langley two-dimensional tunnel at a Reynolds number of about 5,600,000.

Book Pressure Measurements on Two 60   Swept Delta Wings with Blunt Leading Edges and Dihedral Angles of 0   and 45   at a Mach Number of 4 95

Download or read book Pressure Measurements on Two 60 Swept Delta Wings with Blunt Leading Edges and Dihedral Angles of 0 and 45 at a Mach Number of 4 95 written by P. Calvin Stainback and published by . This book was released on 1962 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: