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Author : K. Eyre
Publisher :
ISBN 13 :
Total Pages : 15 pages
Book Rating : 4.:/5 (248 download)
Download or read book Flight Measurements of the pressure distribution on a tempest wing up to a Mach number of o°8 written by K. Eyre and published by . This book was released on 1952 with total page 15 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : K. Eyre
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book Flight Measurements of the Pressure Distribution on a Tempest Wing Up to a Mach Number of 0.8 written by K. Eyre and published by . This book was released on 1946 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Harvey H. Brown
Publisher :
ISBN 13 :
Total Pages : 17 pages
Book Rating : 4.:/5 (64 download)
Download or read book Wing Pressure-distribution Measurements Up to 0.866 Mach Number in Flight on a Jet-propelled Airplane written by Harvey H. Brown and published by . This book was released on 1947 with total page 17 pages. Available in PDF, EPUB and Kindle. Book excerpt: Flight tests were conducted to determine scale and compressibility effects on the pressure distributions over a wing having a NACA low-drag profile. The jet-propelled airplane used permitted tests to be conducted to a Mach number of 0.866.
Author : Lawrence A. Clousing
Publisher :
ISBN 13 :
Total Pages : 21 pages
Book Rating : 4.:/5 (71 download)
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.
Author : United States. National Advisory Committee for Aeronautics
Publisher :
ISBN 13 :
Total Pages : 406 pages
Book Rating : 4.3/5 (243 download)
Download or read book Research Abstracts written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1951 with total page 406 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : H. Arthur Carner
Publisher :
ISBN 13 :
Total Pages : 25 pages
Book Rating : 4.:/5 (11 download)
Download or read book Flight Measurements of the Pressure Distribution on the Wing of the X-1 Airplane (10 Percent Thick Wing) Over a Chordwise Station Near the Midspan, in Level Flight at Mach Numbers from 0.79 to 1.00 and in a Pull-up at a Mach Number of 0.96 written by H. Arthur Carner and published by . This book was released on 1950 with total page 25 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Lawrence A. Clousing
Publisher :
ISBN 13 :
Total Pages : 23 pages
Book Rating : 4.:/5 (773 download)
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:
Author : Lawrence A. Clousing
Publisher :
ISBN 13 :
Total Pages : 42 pages
Book Rating : 4.:/5 (254 download)
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:
Author : Lawrence A. Clousing
Publisher :
ISBN 13 :
Total Pages : 80 pages
Book Rating : 4.:/5 (11 download)
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:
Author : Lawrence A. Clousing
Publisher :
ISBN 13 :
Total Pages : 23 pages
Book Rating : 4.:/5 (11 download)
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:
Author : Aeronautical Research Council (Great Britain)
Publisher :
ISBN 13 :
Total Pages : 912 pages
Book Rating : 4.3/5 (91 download)
Download or read book Technical Report written by Aeronautical Research Council (Great Britain) and published by . This book was released on 1960 with total page 912 pages. Available in PDF, EPUB and Kindle. Book excerpt: Includes its Reports, which are also issued separately.
Author : Marvin Kussoy
Publisher :
ISBN 13 :
Total Pages : 32 pages
Book Rating : 4.:/5 (31 download)
Download or read book Local Pressure Distribution on a Blunt Delta Wing for Angles of Attack Up to 35 Degrees at Mach Numbers of 3.4 and 4.7 written by Marvin Kussoy and published by . This book was released on 1962 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : John A. Zalovcik
Publisher :
ISBN 13 :
Total Pages : 26 pages
Book Rating : 4.3/5 (126 download)
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.
Author : Earl R. Keener
Publisher :
ISBN 13 :
Total Pages : 80 pages
Book Rating : 4.:/5 (31 download)
Download or read book Pressure Measurements Obtained in Flight at Transonic Speeds for a Conically Cambered Delta Wing written by Earl R. Keener and published by . This book was released on 1959 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : P. Calvin Stainback
Publisher :
ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.:/5 (31 download)
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:
Author :
Publisher :
ISBN 13 :
Total Pages : 1356 pages
Book Rating : 4.3/5 (91 download)
Download or read book Aeronautical Engineering Review written by and published by . This book was released on 1952 with total page 1356 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Stavros A. Hartofilis
Publisher :
ISBN 13 :
Total Pages : 68 pages
Book Rating : 4.3/5 (91 download)
Download or read book Pressure Measurement at Mach 19 for a Winged Re-entry Configuration written by Stavros A. Hartofilis and published by . This book was released on 1963 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
