Download or read book Interference of Tail Surfaces and Wing and Fuselage from Tests of 17 Combinations in the N A C A Variable density Tunnel written by Albert Sherman and published by . This book was released on 1939 with total page 110 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Interference of Wing and Fuselage from Tests of 17 Combinations in the N A C A Variable density Tunnel Combinations with Special Junctures written by Albert Sherman and published by . This book was released on 1938 with total page 534 pages. Available in PDF, EPUB and Kindle. Book excerpt: As part of the wing-fuselage interferences investigation in progress in the N.A.C.A. variable-density wind tunnel, a method of eliminating the interference burble associated with critical midwing combinations was investigated. The interference burble of the critical midewing combination was shown to respond to modifications at the nose of the juncture and to be entirely suppressed with little or no adverse effect on the high-speed drag by special leading-edge fillets.
Download or read book Interference of Tail Surfaces and Wing and Fuselage from Tests of 17 Combinations in the N A C A Variable density Tunnel written by Albert Sherman and published by . This book was released on 1939 with total page 10 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Interference of Tail Surfaces and Wing and Fuselage from Tests of 17 Combinations in the NACA Variable density Tunnel written by Albert Sherman and published by . This book was released on 1939 with total page 10 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Interference of Tail Surfaces and Wing and Fuselages from Tests of 17 Combinations in the N A C A Variable density Tunnel written by Albert Sherman and published by . This book was released on 1939 with total page 10 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Report National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1939 with total page 780 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Report written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1939 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Index of Reports on Aeronautical Research written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1940 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Comparison of Vee type and Conventional Tail Surfaces in Combination with Fuselage and Wing in the Variable density Tunnel written by Harry Greenberg and published by . This book was released on 1941 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt: The pitching and yawing moments of a vee-type and a conventional type of tail surface were measured. The tests were made in the presence of a fuselage and a wing-fuselage combination in such a way as to determine the moments contributed by the tail surfaces. The results showed that the vee-type tail tested, with a dihedral angle of 35.3 degrees, was about 71 percent as effective in pitch as the conventional tail and had a yawing-moment to pitching-moment ratio of 0.3. The conventional tail, the panels of which were all congruent to those of the vee-type tail, had a yawing-moment to pitching-moment ratio of 0.48.These ratios are in fair agreement with values calculated by methods shown in this and previous reports. The values of the measured moments were produced from 15 to 25 percent of the calculated value by fuselage interference.
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 1949 with total page 616 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book A Selected Listing of NASA Scientific and Technical Reports for written by and published by . This book was released on 1949 with total page 664 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Annual Report of the National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1938 with total page 828 pages. Available in PDF, EPUB and Kindle. Book excerpt: Includes the Committee's Reports no. 1-1058, reprinted in v. 1-37.
Download or read book Interference of Wing and Fuselage from Tests of 17 Combinations in the NACA Variable density Tunnel written by Albert Sherman and published by . This book was released on 1938 with total page 21 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Catalogue of the Public Documents of the Congress and of All Departments of the Government of the United States for the Period from to written by United States. Superintendent of Documents and published by . This book was released on with total page 3208 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Catalogue of the Public Documents of the the Fifty third Congress to the 76th Congress and of All Departments of the Government of the United States written by United States. Superintendent of Documents and published by . This book was released on 1896 with total page 3208 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Theoretical Lateral Motions of an Automatically Controlled Airplane Subjected to a Yawing moment Disturbance written by Frederick H. Imlay and published by . This book was released on 1941 with total page 546 pages. Available in PDF, EPUB and Kindle. Book excerpt: The lateral motion resulting from a disturbance of the type produced by asymmetric loss of thrust has been determined for a hypothetical average airplane equipped with an automatic pilot. Plots of the resultant motion and the various modes that constitute the motion are presented for controls fixed and for various amounts of automatic control. The automatic control is assumed to be of a type that produces aileron deflections proportional to the angle of bank and rudder deflections proportional to the angle of azimuth. The use of an automatic control may introduce either of two modes. The first mode is primarily a rolling oscillation; the second is a poorly damped long-period oscillation in azimuth and bank . The motion following any change in trim causes the airplane to reach a state of equilibrium on a different flight heading from that existing before the disturbance and the airplane assumes a new flight attitude.
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 1950 with total page 854 pages. Available in PDF, EPUB and Kindle. Book excerpt:
