Download or read book Chordwise Pressure Distribution at High Subsonic Speeds Near Midsemispan of a Tapered 35 Degree Sweptback Wing of Aspect Ratio 4 Having NACA 65A006 Airfoil Sections and Equipped with Various Spoiler Ailerons written by Alexander D. Hammond and published by . This book was released on 1952 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was made in the Langley high-speed 7- by 10-foot tunnel through a Mach number range of 0.60 to 0.93 to determine the effects on the chordwise pressure distributions of projecting various spoiler-type ailerons on a swept wing. The semispan 35 degree sweptback wing had an NACA 65A006 airfoil section, an aspect ratio of 4, and a taper ratio of 0.6.
Download or read book Chordwise Pressures and Section Force and Moment Coefficients at High Subsonic Speeds Near Midspan of a Tapered 35 Degree Sweptback Wing with a Flap type Control and an Attached Tab written by Alexander D. Hammond and published by . This book was released on 1954 with total page 57 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Damping in pitch Characteristics at High Subsonic and Transonic Speeds of Four 35 Sweptback Wings written by William B. Kemp and published by . This book was released on 1953 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book High subsonic Damping in roll Characteristics of a Wing with the Quarter chord Line Swept Back 35 Degrees and with Aspect Ratio 3 and Taper Ratio 0 6 written by Boyd C. II. Myers and published by . This book was released on 1949 with total page 21 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Chordwise and Spanwise Loadings Measured at a Large Triangular Wing Having an Aspect Ratio of 2 and a Thin Subsonic type Airfoil Section written by and published by . This book was released on 1950 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Supersonic Lift and Pitching Moment of Thin Sweptback Tapered Wings Produced by Constant Vertical Acceleration written by Frank S. Malvestuto and published by . This book was released on 1951 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: Design curves are presented which permit rapid estimations of lift and pitching moment for given values of aspect ratio, taper ratio, Mach number, and leading-edge sweep.
Download or read book Theoretical Lift and Damping in Roll of Thin Sweptback Wings of Arbitrary Taper and Sweep at Supersonic Speeds written by Frank S. Malvestuto and published by . This book was released on 1949 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt: Design curves are presented which permit rapid estimation of the lift-curve slope and damping-in-roll derivative for given values of aspect ratio, taper ratio, Mach number, and leading edge sweep.
Download or read book The Calculation of Downwash Behind Supersonic Wings with an Application to Triangular Plan Forms written by Max A. Heaslet and published by . This book was released on 1948 with total page 726 pages. Available in PDF, EPUB and Kindle. Book excerpt: A method is developed, consistent with the assumptions of small perturbation theory, which provides a means of determining for a known load distribution, the downwash behind a wing in supersonic flow. THe analysis is based upon the use of supersonic doublets which are distributed over the plan form and wake of the wing in a manner determined from the wing loading.
Download or read book Factors Affecting the Maximum Lift drag Ratio at High Supersonic Speeds written by Charles H. McLellan and published by . This book was released on 1956 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt: A study of the factors affecting the maximum lift-drag ratio has been conducted in an effort to determine how to obtain high aerodynamic values at high supersonic Mach numbers.
Download or read book The Theoretical Supersonic Pressure Distribution Over Tapered Sweptback Wings with Arbitrary Airfoil Sections written by W. R. Laster and published by . This book was released on 1948 with total page 19 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Low speed Characteristics in Pitch of a 42 Degrees Sweptback Wing with Aspect Ratio 3 9 and Circular arc Airfoil Sections written by Robert H. Neely and published by . This book was released on 1947 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Experimental Investigation of the Pressure Distribution at the Centre section of a Sweptback Wing at High Subsonic Speeds written by Aeronautical Research Council and published by . This book was released on 1957 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Low speed Characteristics of a 45 Degrees Sweptback Wing of Aspect Ratio 8 from Pressure Distributions and Force Tests at Reynolds Numbers from 1 500 000 to 4 800 000 written by Robert R. Graham and published by . This book was released on 1951 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effects of the Spanwise Chordwise and Vertical Location of an External Store on the Aerodynamic Characteristics of a 45 Degree Sweptback Tapered Wing of Aspect Ratio 4 at Mach Numbers of 1 41 1 62 and 1 96 written by Carl R. Jacobsen and published by . This book was released on 1953 with total page 31 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Damping in pitch Characteristics at High Subsonic and Transonic Speeds of Four 35 Degree Sweptback Wings written by William B. Jr Kemp and published by . This book was released on 1953 with total page 21 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Damping of Straight and 45 Degrees Swept Wings of Various Taper Ratios Determined at High Subsonic Transonic and Supersonic Speeds with Rocket powered Models written by E. Claude Jr Sanders and published by . This book was released on 1951 with total page 15 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Lift and Stalling Characterisitcs of a 35 Degrees Swept Back Wing Designed to Have Identical Chordwise Pressure Distributions at All Spanwise Stations when Near Maximum Lift written by D.S. Woodward and published by . This book was released on 1971 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt:
