Download or read book Interference Between the Wings and the Tailplane of a Slender Wing body tailplane Combination written by P.R. Owen and published by . This book was released on 1951 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Interference Between the Wings and the Tail Surfaces of a Combination of Slender Body Cruciform Wings and Cruciform Tail Set at Both Incidence and Yaw written by P.R. Owen and published by . This book was released on 1952 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Aerodynamic Interference of Slender Wing tail Combinations written by Alvin H. Sacks and published by . This book was released on 1956 with total page 81 pages. Available in PDF, EPUB and Kindle. Book excerpt: Mathematical expressions are derived for the interference forces and moments acting on the tails of slender plane and cruciform wing-tail combinations of general plan form in steady straight flight at combined angles of attack and sideslip. The derivatives are made within the limitations of slender-body theory under the assumption that the vortex sheet leaves the wing as flat sheet and becomes fully rolled up ahead of the tail. The derived expressions are used to calculate the steady lifts, side forces, pitching moments, and rolling moments of the number of wing-tail combinations. The effects of changes in tail height, tail length, ratio of tail span to wing span, tail incidence, and tail thickness are calculated. The resulting curves, and particularly their nonlinearities, are discussed at some length in connection with static stability. In general, the most dramatic effects are noted when the vortices shed from the wing strike the tips of the tail trailing edge.

Download or read book Current Papers written by and published by . This book was released on 1963 with total page 846 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Technical Report written by Aeronautical Research Council (Great Britain) and published by . This book was released on 1971 with total page 684 pages. Available in PDF, EPUB and Kindle. Book excerpt: Includes its Reports, which are also issued separately.

Download or read book Report written by and published by . This book was released on 1959 with total page 922 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Report written by North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development and published by . This book was released on 1959 with total page 684 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Journal of the Royal Aeronautical Society written by and published by . This book was released on 1956 with total page 976 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book The Journal of the Royal Aeronautical Society written by Royal Aeronautical Society and published by . This book was released on 1956 with total page 962 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Reports and Memoranda written by and published by . This book was released on 1962 with total page 1028 pages. Available in PDF, EPUB and Kindle. Book excerpt: Beginning with no. 650 each hundredth number contains a list of the Reports and memoranda published since the last list.

Download or read book Aerodynamic Interference Between a Wing and a Slender Cylindrical Store written by Paul M. Sullivan and published by . This book was released on 1971 with total page 89 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aerodynamic interference between an aircraft and a store carried beneath its wing is investigated using the simplified physical model of a uniform wing of infinite span and a slender body of revolution positioned beneath the wing. The wing is represented by a vortex filament, the store by a distribution of sources and doublets along its axis of revolution, and potential flow is presumed to exist. The aerodynamic forces acting on the store while it is attached to the aircraft are computed using this model. The trajectory that the store follows after it is released is studied for mass, initial position relative to the wing, and initial angle of attack. If a store is symmetric and homogeneous, it appears to be unstable after release, and rapidly violates the small angle assumptions of the study. Several trajectories are computed, and show that the aerodynamic loads can be large enough to propel a store of considerable mass into the ai craft that released it.

Download or read book Results and Analysis of Pressure Measurements on Two Isolated Slender Wings and Slender Wingbody Combinations at Supersonic Speeds written by K. A. Fellows and published by . This book was released on 1969 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Wind tunnel Investigation of a Number of Total pressure Tubes at High Angles of Attack written by A. Gerald Rainey and published by . This book was released on 1957 with total page 316 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Reports and Memoranda Aeronautical Research Council written by Aeronautical Research Council (Great Britain) and published by . This book was released on 1955 with total page 860 pages. Available in PDF, EPUB and Kindle. Book excerpt: Beginning with no. 650 each hundredth number contains a list of the Reports and memoranda published since the last list.

Download or read book Factors Determining the Performance of Indexing Systems written by Cyril W. Cleverdon and published by . This book was released on 1966 with total page 272 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book An Investigation of Wing body Juncture Interference Effects at Transonic Speeds for Several Swept wing and Body Combinations written by John B. McDevitt and published by . This book was released on 1957 with total page 107 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report presents the results of an investigation of wing-body juncture interference effects at high subsonic and transonic speeds. Force characteristics and pressure measurements for various bodies in combination with sweptback wings of aspect ratios 3 and 6 were obtained through a Mach number range from 0.8 to 1.2. The bodies used consisted of basic Sears-Haack bodies of revolution, the basic bodies indented by area-rule concepts at design Mach numbers of 1.0 and 1.2, and the latter area-rule bodies reshaped without-change in cross-sectional areas (by the superposition of slender-body multiples) so that the flow along the wing-body juncture chords at high subsonic speeds more closely resembled that for the infinite oblique wing.

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.