Download or read book The Effect at High Subsonic Speeds of a Flap type Aileron on the Chordwise Pressure Distribution Near Midsemispan of a Tapered 35 Degree Sweptback Wing of Aspect Ratio 4 Having NACA 65A006 written by Homer B. Wilson and published by . This book was released on 1953 with total page 89 pages. Available in PDF, EPUB and Kindle. Book excerpt: This paper presents effects of the deflection of a flat-type aileron on the chordwise pressure distribution at the 46-percent-semispan station of a tapered 35 degree sweptback wing of aspect ratio 4 with an NACA 65A006 airfoil section. The tests were made at angles of attack from 0 to 20 degrees and at Mach numbers from 0.60 to 0.95 for aileron deflections from -30 to 30 degrees.
Download or read book The Effect at High Subsonic Speeds of a Flap type Aileron on the Chordwise Pressure Distribution Near Midspan of a Tapered 35 Degree Sweptback Wing of Aspect Ratio 4 Having NACA 65A006 Airfoil Section written by Alexander D. Hammond and published by . This book was released on 1953 with total page 89 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Pressure Distribution on Plug and Semaphore type Spoiler Ailerons on a 35 Degree Sweptback Wing of Aspect Ratio 4 Taper Ratio 0 6 and NACA 65A006 Airfoil Section at High Subsonic Speeds written by Alexander D. Hammond and published by . This book was released on 1954 with total page 55 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Pressure Distributions on Plug and Semaphore type Spoiler Ailerons on a 35 sweptback Wing of Aspect Ratio 4 Taper Ratio 0 6 and NACA 65A006 Airfoil Section at High Subsonic Speeds written by Alexander D. Hammond and published by . This book was released on 1954 with total page 55 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Journal of Aircraft written by and published by . This book was released on 1972 with total page 528 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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 The Twisting Effect at Transonic Speeds of Spoiler Ailerons on a 45 Sweptback Aspect ratio 4 Tapered Wing written by Alexander D. Hammond and published by . This book was released on 1954 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Twisting Effects at Transonic Speeds of Spoiler Ailerons on a 45 Degree Sweptback Aspect ratio 4 Tapered Wing written by Alexander D. Hammond and published by . This book was released on 1954 with total page 21 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effect of a Wing Leading edge Flap and Chord extension on the High Subsonic Control Characteristics of an Aileron Located at Two Spanwise Positions written by Robert F. Thompson and published by . This book was released on 1955 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation at High Subsonic Speeds of the Effect of Horizontal tail Location on Longitudinal and Lateral Stability Characteristics of a Complete Model Having a Sweptback Wing in a High Location written by H. Norman Silvers and published by . This book was released on 1956 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was made at high subsonic speeds of the longitudinal and lateral stability of a complete model having four vertical locations of the horizontal tail and a sweptback wing located in a high position on the fuselage. The wing had 45 degrees of sweepback, an aspect ratio of 4.0, and a taper ratio of 0.3. The results were obtained in the Langley high-speed 7- by 10-foot tunnel at Mach numbers from 0.80 to 0.92.
Download or read book The Forces and Pressure Distribution at Subsonic Speeds on a Cambered and Twisted Wing Having 45 Degrees of Sweepback an Aspect Ratio of 3 and a Taper Ratio of 0 5 written by Frederick W. Boltz and published by . This book was released on 1952 with total page 166 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 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 The Forces and Pressure Distribution at Subsonic Speeds on a Plane Wing Having 45 Degrees of Sweepback an Aspect Ratio of 3 and a Taper Ratio of 0 5 written by Carl D. Kolbe and published by . This book was released on 1951 with total page 159 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation of Aerodynamic Characteristics in Pitch and Sideslip of a 45 Degree Sweptback wing Airplane Model with Various Vertical Locations of Wing and Horizontal Tail written by M. Leroy Spearman and published by . This book was released on 1956 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been conducted in the Langley 4- by 4-foot supersonic pressure tunnel to determine the effects of various vertical locations of the wing and horizontal tail on the aerodynamic characteristics in pitch of a supersonic airplane configuration at a Mach number of 2.01. The model is equipped with a wing and horizontal tail, each having a 45 degree sweep and an aspect ratio of 4. The wing had a taper ratio of 0.2 with NACA 65A004 airfoil sections, whereas the horizontal tail had a taper ratio of 0.6 with NACA 65A006 airfoil sections.
Download or read book The Subsonic Static Aerodynamic Characteristics of an Airplane Model Having a Triangular Wing of Aspect Ratio 3 written by Howard F. Savage and published by . This book was released on 1957 with total page 662 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been conducted to determine the effects of vertical-tail location and size on the subsonic aerodynamic characteristics of a model having a triangular wing. The wing had an aspect ratio of 3, an NACA 0003.5-63 section in the streamwise direction, and plain, trailing-edge ailerons. The wing was attached to the fuselage in either a mid or high position and an unswept horizontal tail was located on the fuselage center line. Two vertical tails were tested which had areas of 26.7 or 20.3 percent of the wing area. Each vertical tail was equipped with a rudder and had a geometric aspect ratio of 1.5, a taper ratio of 0.16, and 54 degrees of sweepback of the leading edge. Each vertical tail was tested at two different tail lengths. The wind-tunnel tests were conducted at a Reynolds number of 2.5 milMon at Mach numbers from 0.25 to 0.95.
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.
