Download or read book Tests in the Ames 40 by 80 foot Wind Tunnel of the Aerodynamic Characteristics of Airplane Models with Spoiler Ailerons written by Ralph W. Franks and published by . This book was released on 1954 with total page 47 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Tests in the Ames 40 by 80 foot Wind Tunnel of an Airplane Configuration with an Aspect Ratio 2 Triangular Wing and an All movable Horizontal Tail Lateral Characteristics written by David Graham and published by . This book was released on 1952 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aerodynamic Characteristics of the Modified 40 by 80 foot Wind Tunnel as Measured in a 1 50th scale Model written by and published by . This book was released on 1987 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book WADC Technical Report written by United States. Wright Air Development Division and published by . This book was released on 1957 with total page 1268 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Tests of an Attack type Airplane in the Ames 40 by 80 foot Wind Tunnel to Improve the High speed Maneuvering Control force Characterstics written by Gerald M. McCormack and published by . This book was released on 1945 with total page 37 pages. Available in PDF, EPUB and Kindle. Book excerpt: Wind-tunnel tests were made of a twin-engine airplane to determine modifications which would make the airplane suitable for ground-support attack operations. It was desired to reduce the high-speed elevator and aileron control forces without either reducing the low-speed control forces or impairing the landing characteristics.
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 1956 with total page 580 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1985 with total page 1346 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Full scale Wind tunnel Tests of a Small Unpowered Jet Aircraft with a T Tail written by Paul T. Soderman and published by . This book was released on 1971 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt: The aerodynamic characteristics of a full scale executive type jet transport aircraft with a T-tail were investigated in a 40 x 80 ft (12.2 by 24.4 meter) wind tunnel (subsonic). Static, longitudinal, and lateral stability, and control characteristics were determined at angles of attack from -2 deg to 42 deg. The aircraft wing had 13 deg of sweep and an aspect ratio of 5.02. The aircraft was tested power off with various wing leading- and trailing-edge high lift devices. The basic configuration was tested with and without such components as engine nacelles, wing tip tanks, and empannage. Hinge-moment data were obtained and downwash angles in the horizontal-tail plane location were calculated. The data were obtained at Reynolds numbers of 4.1 million and 8.7 million based on mean aerodynamic chord. The model had static longitudinal stability through initial stall. Severe tail buffet occurred near the angle of attack for maximum lift. Above initial stall the aircraft had pronounced pitch-up, characteristic of T-tail configurations. A stable trim point was possible at angles of attack between 30 deg and 40 deg (depending on c.g. location and flap setting). Hinge-moment data showed no regions with adverse effects on stick force. Comparisons of wind-tunnel data and flight-test are presented.
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 Technical Note written by and published by . This book was released on 1973 with total page 410 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Subject Index to Unclassified ASTIA Documents written by Defense Documentation Center (U.S.) and published by . This book was released on 1960 with total page 894 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Tests in the Ames 40 by 80 foot Wind Tunnel of an Airplane Configuration with an Aspect Ratio 4 Triangular Wing and an All movable Horizontal Tail Longitudinal Characteristics written by David Graham and published by . This book was released on 1951 with total page 27 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Tests in the Ames 40 by 80 foot Wind Tunnel of an Airplane Model with an Aspect Ratio 4 Triangular Wing and an All movable Horizontal Tail High lift Devices and Lateral Controls written by Ralph W. Franks and published by . This book was released on 1953 with total page 45 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Tests in the Ames 40 by 80 foot Wind Tunnel of an Airplane Configuration with an Aspect Ratio 3 Triangular Wing and an All movable Horizontal Tail Longitudinal and Lateral Characteristics written by David G. Koenig and published by . This book was released on 1953 with total page 61 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Use of the Horizontal Tail for Roll Control written by John P. Campbell and published by . This book was released on 1956 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Research Abstracts and Reclassification Notice written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1956 with total page 716 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Scientific and Technical Reports written by United States. National Aeronautics and Space Administration Scientific and Technical Information Division and published by . This book was released on 1966 with total page 1440 pages. Available in PDF, EPUB and Kindle. Book excerpt:
