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Masurements In Flight Of The Pressure Distribution On The Right Wing Of A Pursuit Type Airplane At Several Values Of Mach Number
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Book Synopsis Measurements in Flight of the Pressure Distribution on the Right Wing of a Pursuit-type Airplane at Several Values of Mach Number by : Lawrence A. Clousing
Download or read book Measurements in Flight of the Pressure Distribution on the Right Wing of a Pursuit-type Airplane at Several Values of Mach Number written by Lawrence A. Clousing and published by . This book was released on 1946 with total page 23 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Measurements in Flight of the Pressure Distribution on the Right Wing of a Pursuit-type Airplane at Several Values of Mach Number by : Lawrence A. Clousing
Download or read book Measurements in Flight of the Pressure Distribution on the Right Wing of a Pursuit-type Airplane at Several Values of Mach Number written by Lawrence A. Clousing and published by . This book was released on 1949 with total page 23 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Masurements in Flight of the Pressure Distribution on the Right Wing of a Pursuit - Type Airplane at Several Values of Mach Number by : Lawrence A. Clousing
Download or read book Masurements in Flight of the Pressure Distribution on the Right Wing of a Pursuit - Type Airplane at Several Values of Mach Number written by Lawrence A. Clousing and published by . This book was released on 1946 with total page 23 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Report by : United States. National Advisory Committee for Aeronautics
Download or read book Report written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1946 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Technical Information Pilot written by and published by . This book was released on 1949 with total page 694 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1950 with total page 578 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Measurements in Flight of the Pressure Distribution on the Right Wing of a P-39N-1 Airplane at Several Values of Mach Power by : Lawrence A. Clousing
Download or read book Measurements in Flight of the Pressure Distribution on the Right Wing of a P-39N-1 Airplane at Several Values of Mach Power written by Lawrence A. Clousing and published by . This book was released on 1945 with total page 21 pages. Available in PDF, EPUB and Kindle. Book excerpt: Pressure-distribution measurements were made on the right wing of a P-39N-1 airplane at values of Mach number up to 0.80. The results showed that a considerable portion of the lift was carried by components of the airplane other than the wings, and that the proportion of lift carried by the wings may vary considerably with Mach number, thus changing the bending moment at the wing root whether or not there is a shift in the lateral position of the center of pressure. It was also shown that the center of pressure does not necessarily move outward at high Mach numbers, even though the wing-thickness ratio decreases toward the wing tip. The wing pitching-moment coefficient increased sharply in a negative direction at a Mach number slightly higher than the critical Mach number. The lift-curve slope increased with Mach number which, in some instances, were considerably above the critical value. Pressures inside the wing were small and negative.
Book Synopsis Report - National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics
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 1946 with total page 516 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Measurements in Flight of the Pressure Distribution on the Right Wing of a P-39N-1 Airplane at Several Values of Mach Number by : Lawrence A. Clousing
Download or read book Measurements in Flight of the Pressure Distribution on the Right Wing of a P-39N-1 Airplane at Several Values of Mach Number written by Lawrence A. Clousing and published by . This book was released on 1945 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Flight Investigation at High Mach Numbers of Several Methods of Measuring Static Pressure on an Airplane Wing by : John A. Zalovcik
Download or read book Flight Investigation at High Mach Numbers of Several Methods of Measuring Static Pressure on an Airplane Wing written by John A. Zalovcik and published by . This book was released on 1944 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt: Summary: A flight investigation was made to compare static pressures in subsonic and supersonic flow over an airplane wing as measured by static-pressure tubes, a static-pressure belt, and orifices flush with the wing surface. The measurements were made on the upper surface of the wing of the P-47D airplane over a range of flight conditions in which local Mach numbers from 0.34 to 1.41 were obtained at the measurement stations. For some of the tests, a total-pressure tube was mounted on the wing surface to determine its characteristics in supersonic flow. The results indicated that static-pressure measurements obtained with suitably designed and installed flush orifices, static-pressure tubes, and static-pressure belt will be in reasonable agreement for both subsonic and supersonic flow. The pressures in supersonic flow measured by the total-pressure tube mounted on the wing surface were found to be in close agreement with values predicted by theory.
Book Synopsis Charts of Pressure Rise Obtainable with Airfoil-type Axial-flow Cooling Fans by : A. Kahane
Download or read book Charts of Pressure Rise Obtainable with Airfoil-type Axial-flow Cooling Fans written by A. Kahane and published by . This book was released on 1947 with total page 578 pages. Available in PDF, EPUB and Kindle. Book excerpt: Charts are presented to show the pressure rise that is obtainable in an engine-cooling installation with a typical airfoil-type propeller-speed fan. The charts cover fans of the stator-rotor, rotor-stator, and rotor alone configurations, with blades incorporating both the highly cambered 65-series blower-blade sections and the conventional low-cambered airfoil sections. The effects of operation of a geared fan with rotational speeds limited by compressibility considerations and the effects of initial rotational inflow are indicated. Use of the charts to predict the pressure rise obtainable with any fan of the types considered is illustrated in a sample calculation.
Book Synopsis Annual Report of the National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics
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 1945 with total page 512 pages. Available in PDF, EPUB and Kindle. Book excerpt: Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Book Synopsis Measurement in Flight of the Pressure Distribution on the Right Wing of a P-39N-1 Airplane at Several Values of Mach Number by : Lawrence A. Clousing
Download or read book Measurement in Flight of the Pressure Distribution on the Right Wing of a P-39N-1 Airplane at Several Values of Mach Number written by Lawrence A. Clousing and published by . This book was released on 1945 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Index of NACA Technical Publications by : United States. National Advisory Committee for Aeronautics
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:
Book Synopsis A Selected Listing of NASA Scientific and Technical Reports for ... by :
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 NASA SP. written by and published by . This book was released on 1962 with total page 130 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Measurements of the Pressure Distribution on the Horizontal-tail Surface of a Typical Propeller-driven Pursuit Airplane in Flight by : Melvin Sadoff
Download or read book Measurements of the Pressure Distribution on the Horizontal-tail Surface of a Typical Propeller-driven Pursuit Airplane in Flight written by Melvin Sadoff and published by . This book was released on 1947 with total page 29 pages. Available in PDF, EPUB and Kindle. Book excerpt: Pressure-distribution measurements were made in steady straight and accelerated flight over both sides of the horizontal-tail surface of a typical pursuit airplane up to a Mach number of 0.79. The results showed that a sharply increasing down-load was required to balance the increased diving moment of the wing-fuselage-propeller group at Mach numbers above about 0.70. There was little change, up to a Mach number of about 0.65, of the tail-load gradient (rate of increase of tail load for a unit change in acceleration factor); beyond that Mach number, however, a rapid decrease of tail-load gradient to a Mach number of about 0.73 and then a very sharp increase up to a Mach number of 0.785 was noted. The root bending moments increased considerably on the right tail and decreased, to a lesser extent, on the left tail at the higher Mach numbers, resulting in increased fuselage torsional moments at high speeds. At the higher values of lift coefficient (0.5 to 0.8), there was little change of the lateral distance to the center pressure up to a Mach number of about 0.73; at the highest speed and at low lift coefficients (0 to 0.1) the center of pressure was inboard approximately 3 feet on the left tail and 1.5 feet on the right tail as compared with the values at lower speeds. It appears that satisfactory quantitative data on total tail loads may be obtained from measurements at four stations, equally spaced along the entire tail span.
