Download or read book Note on the Longitudinal Stability and Trim of Tailless Aircraft written by A. W. Thorpe and published by . This book was released on 1942 with total page 15 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Notes on the Stability and Control of Tailless Airplanes written by Robert Thomas Jones and published by . This book was released on 1941 with total page 12 pages. Available in PDF, EPUB and Kindle. Book excerpt: Problems involved in the stability and control of tailless airplanes are discussed. Such factors as the location of the aerodynamic center and its effect on the longitudinal stability, longitudinal trim with high-lift devices, the effects of various changes in the shape of the wing on lateral stability, and the effects of nacelles are covered.

Download or read book Effect of Wing Modifications on the Longitudinal Stability of a Tailless All wing Airplane Model written by Charles L. Seacord and published by . This book was released on 1945 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt: Summary: An investigation of the power-off longitudinal stability characteristics of a tailless all-wing airplane model with various wing modifications has been made in the Langley free-flight tunnel. Force and tuft tests were made on the model in the original condition, with the wing tips rotated for washout, with rectangular and swept-forward tips, and with various slat arrangements. Flight tests were made with the original wing and with the original wing equipped with the most promising modifications. The results indicated that changes in tip plan form or rotation of the wing tips did not appreciably reduce the instability at high lift coefficients. Addition of wing slats, however, improved the longitudinal stability at the stall when the slat extended far enough inboard to cover the area that tended to stall first.

Download or read book Longitudinal Stability and Trim of Two Rocket propelled Airplane Models Having 45 Sweptback Wings and Tails with the Horizontal Tail Mounted in Two Positions written by James H. Parks and published by . This book was released on 1953 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Notes on the Static Longitudinal Stability and Control of Aircraft written by Waldemar Otto Brehaus and published by . This book was released on 1953 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Analysis of the Longitudinal Stability of Tailless and Tail first Aircraft written by S. Neumark and published by . This book was released on 1944 with total page 75 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book The Longitudinal Controls Fixed Static Stability of Tailless Aircraft written by Cranfield Institute of Technology. College of Aeronautics and published by . This book was released on 2000 with total page 25 pages. Available in PDF, EPUB and Kindle. Book excerpt: This paper describes the development of a simple theory of the longitudinal controls fixed static stability of tailless aeroplanes. The classical theory, as developed for the conventional aircraft, is modified to accommodate the particular features of the tailless aeroplanes. The theory was then applied to a particular blended-wing-body tailless civil transport aircraft, BWB-98.

Download or read book Notes on Longitudinal Stability and Balance written by Edward Pearson Warner and published by . This book was released on 1920 with total page 630 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book A Note on the Drag Due to Lift of Delta Wings at Mach Numbers Up to 2 0 written by Robert S. Osborne and published by . This book was released on 1960 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book General Considerations Concerning the Longitudinal Stability and Control of Tailless Aircraft series 1 written by A. J. Marx and published by . This book was released on 1950 with total page 208 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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 1146 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 1972 with total page 602 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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 1933 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book The Static and Dynamic Longitudinal Stability Characteristics of Some Supersonic Aircraft Configurations written by Jesse L. Mitchell and published by . This book was released on 1952 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book The Study of the Static Longitudinal Stability of a Tailless Airplane written by Robert Sanders and published by . This book was released on 1931 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book The Longitudinal Static Stability of Tailless Aircraft written by H. V. De Castro and published by . This book was released on 2001 with total page 47 pages. Available in PDF, EPUB and Kindle. Book excerpt: This paper describes the development of a simple theory of the longitudinal controls fixed static stability of tailless aeroplanes. The classical theory, as developed for the conventional aircraft, is modified to accommodate the particular features of the tailless aeroplanes. The theory was then applied to a particular blended-wing-body tailless civil transport aircraft, BWB-98.

Download or read book Analysis of Longitudinal Stability and Trim of the Bell X 1 Airplane at a Lift Coefficient of 0 3 to Mach Numbers Near 1 05 written by Hubert M. Drake and published by . This book was released on 1951 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt: