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The Aerodynamic Characteristics Of Wrap Around Fins At Mach Numbers Of 03 To 30
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Book Synopsis The Aerodynamic Characteristics of Wrap-around Fins at Mach Numbers of 0.3 to 3.0 by : C. Wayne Dahlke
Download or read book The Aerodynamic Characteristics of Wrap-around Fins at Mach Numbers of 0.3 to 3.0 written by C. Wayne Dahlke and published by . This book was released on 1976 with total page 61 pages. Available in PDF, EPUB and Kindle. Book excerpt: Results of investigations into many of the geometric and flow parameters influencing the aerodynamics of wrap-around fins are presented in this report. Particular emphasis is placed on defining static and dynamic roll characteristics between Mach numbers of 0.3 to 3.0. Among the geometric parameters highlighted are fin span, aspect ratio, leading edge sweep, leading edge shape, fin opening angle, and afterbody geometry. Comparisons of static stability, dynamic stability, and drag are made between the flat and the wrap- around fin. Problems associated with measurement of wrap-around fin rolling mounts are also discussed. An overview of the wrap-around fin roll moment characteristics are presented as an aid for making estimates and establishing testing techniques. This report supercedes RD-73-17.
Book Synopsis The Aerodynamic Characteristics of Wrap-Around Fins, Including Fold Angle at Mach Numbers from 0.5 to 1.3 by : C. W. Dahlke
Download or read book The Aerodynamic Characteristics of Wrap-Around Fins, Including Fold Angle at Mach Numbers from 0.5 to 1.3 written by C. W. Dahlke and published by . This book was released on 1974 with total page 517 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation was conducted in the transonic wind tunnel to study the aerodynamic characteristics of wrap-around fins. Wrap-around fins with leading edge sweep angle on straight and step down bodies were tested. One unswept fin was tested simulating various opening angles from 10 degrees beyond fully open to a folding angle of 112.5 degrees. Force and moment data were obtained at Mach numbers from 0.5 to 1.3 at angles of attack up to 14 degrees and roll angles from 0 to 67.5 degrees. The results of the test are presented in plotted form for the main balance and all four fin balances.
Book Synopsis A Summary of Aerodynamic Characteristics for Wrap-around Fins from Mach 0.3 to 3.0 by : James A. Humphrey
Download or read book A Summary of Aerodynamic Characteristics for Wrap-around Fins from Mach 0.3 to 3.0 written by James A. Humphrey and published by . This book was released on 1977 with total page 234 pages. Available in PDF, EPUB and Kindle. Book excerpt: Wrap-around fin effectiveness for tube-launched missiles was investigated in a series of 6 wind tunnel tests. Wind tunnels were AEDC Propulsion Wind Tunnel, NASA/Langley Research Center Unitary Plan Wind Tunnel and McDonnell Douglas 4-foot Trisonic Wind Tunnel. Mach number range was 0.3 to 3.0. Basic model was a 2-caliber secant ogive nose with an 8-caliber cylindrical afterbody and 21 fin configurations. Variations in the coefficients are presented for changes in fin geometry including taper ratio and leading edge sweep angle, aspect ratio, exposed semi-span, and root chord length; opening angle, fully closed to 10 deg past fully open; and body step down.
Book Synopsis The Aerodynamic Characteristics of Wrap-Around Fins, Including Fold Angle at Mach Numbers from 0.5 to 3.0 by : C. W. Dahlke
Download or read book The Aerodynamic Characteristics of Wrap-Around Fins, Including Fold Angle at Mach Numbers from 0.5 to 3.0 written by C. W. Dahlke and published by . This book was released on 1974 with total page 367 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation was conducted in the McDonnell Douglas Aerophysics Laboratory 4-foot trisonic wind tunnel to study the aerodynamic characteristics of wrap around fins. Wrap around fins with leading edge sweep angle and exposed semi-span variations were tested. One unswept fin was tested simulating various opening angles from 10 degrees beyond fully open to a folding angle of 112.5 degrees. Force and moment data were obtained at Mach Numbers from 0.5 to 3.0 at angles of attack up to 14 degrees and roll angles from 0 to 45 degrees. The complete results of this test are presented in plotted form for the main balance and all four fin balances.
Book Synopsis Aerodynamic Characteristics of Wraparound Fins Mounted on Bodies of Revolution and Their Influence on the Missile Static Stability at Mach Numbers from 0.3 to 1.3. Volume I. by :
Download or read book Aerodynamic Characteristics of Wraparound Fins Mounted on Bodies of Revolution and Their Influence on the Missile Static Stability at Mach Numbers from 0.3 to 1.3. Volume I. written by and published by . This book was released on 1972 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: AMCDR-1001-Vol-1See also Volume 2, AD-772 670.*Guided missiles, *Fins, Tube launched, Aerodynamic forces, Pitch(Motion), Roll, Yaw, Angle of attackWraparound finsExperimental aerodynamic investigations were conducted for several wraparound fins and one planar fin configuration on bodies of revolution at Mach number ranging from 0.3 to 1.3 and angles of attack from -6 degrees to 6 degrees at 0 degrees at sideslip angle. Six component aerodynamic forces and moments were recorded on the complete missile configuration while simultaneously measuring the aerodynamic normal force and bending moments acting on each fin. The fin configuration parameters varied include chord length, fin thickness, leading edge configuration, tip chord geometry and body, root chord gap. The report presents the plotted coefficient data in two volumes. Volume I contains the complete missile aerodynamic data. (Modified author abstract).
Book Synopsis Aerodynamic Characteristics of Wraparound Fins Mounted on Bodies of Revolution and Their Influence on the Missile Static Stability at Mach Numbers from 0.3 to 1.3. Volume II. by :
Download or read book Aerodynamic Characteristics of Wraparound Fins Mounted on Bodies of Revolution and Their Influence on the Missile Static Stability at Mach Numbers from 0.3 to 1.3. Volume II. written by and published by . This book was released on 1972 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: OL-2AMCDR-1001-Vol-2See also Volume 1, AD-772 669.*Guided missiles, *Fins, Tube launched, Aerodynamic forces, Pitch(Motion), Roll, Yaw, Angle of attackWraparound finsExperimental aerodynamic investigations were conducted for several wraparound fins and one planar fin configuration on bodies of revolution at Mach number ranging from 0.3 to 1.3 and angles of attack from -6 degrees to 6 degrees at 0 degrees sideslip angle. Six component aerodynamic forces and moments were recorded on the complete missile configuration while simultaneously measuring the aerodynamic normal force and bending moments acting on each fin. The fin configuration parameters varied include chord length, fin thickness, leading edge configuration, tip chord geometry and body, root chord gap. The report presents the plotted coefficient data in two volumes. Volume 2 contains the individual fin aerodynamic data. (Modified author abstract).
Book Synopsis The Aerodynamic Characterictics of Wrap-around Fins at Mach Numbers of 0.3 to 3.0 by : C. W. Dahlke
Download or read book The Aerodynamic Characterictics of Wrap-around Fins at Mach Numbers of 0.3 to 3.0 written by C. W. Dahlke and published by . This book was released on 1976 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of Several Low Aspect Ratio Stabilizer Fins at Mach Numbers from 0.8 to 1.3 by : J. M. Whoric
Download or read book Aerodynamic Characteristics of Several Low Aspect Ratio Stabilizer Fins at Mach Numbers from 0.8 to 1.3 written by J. M. Whoric and published by . This book was released on 1972 with total page 154 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of Low Aspect Ratio Fins at Mach Numbers from 0.80 to 1.30 by : D.K. Smith
Download or read book Aerodynamic Characteristics of Low Aspect Ratio Fins at Mach Numbers from 0.80 to 1.30 written by D.K. Smith and published by . This book was released on 1971 with total page 166 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of Wraparound Fins Mounted on Bodies of Revolution and Rheir Influence on the Missile Static Stability at Mach Numbers from 0.3 to 1.3 by : Calvin Wayne Dahlke
Download or read book Aerodynamic Characteristics of Wraparound Fins Mounted on Bodies of Revolution and Rheir Influence on the Missile Static Stability at Mach Numbers from 0.3 to 1.3 written by Calvin Wayne Dahlke and published by . This book was released on 1972 with total page 376 pages. Available in PDF, EPUB and Kindle. Book excerpt: Experimental aerodynamic investigations were conducted for several wraparound fins and one planar fin configuration on bodies of revolution at Mach number ranging from 0.3 to 1.3 and angles of attack from -6 degrees to 6 degrees at 0 degrees at sideslip angle. Six component aerodynamic forces and moments were recorded on the complete missile configuration while simultaneously measuring the aerodynamic normal force and bending moments acting on each fin. The fin configuration parameters varied include chord length, fin thickness, leading edge configuration, tip chord geometry and body, root chord gap. The report presents the plotted coefficient data in two volumes. Volume I contains the complete missile aerodynamic data. Volume 2 contains the individual fin aerodynamic data.
Book Synopsis Aerodynamic Test and Analysis of Wrap-around Fins at Supersonic Mach Numbers Utilizing Design of Experiments by : Mark W. Swenson
Download or read book Aerodynamic Test and Analysis of Wrap-around Fins at Supersonic Mach Numbers Utilizing Design of Experiments written by Mark W. Swenson and published by . This book was released on 1994 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of Low Aspect Ratio Fins at Mach Numbers from 0.80 to 1.30 by : D.K. Smith
Download or read book Aerodynamic Characteristics of Low Aspect Ratio Fins at Mach Numbers from 0.80 to 1.30 written by D.K. Smith and published by . This book was released on 1971 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Effect of Wrap-around Fins on Aerodynamic Stability and Rolling Moment Variations by : C. W. Dahlke
Download or read book The Effect of Wrap-around Fins on Aerodynamic Stability and Rolling Moment Variations written by C. W. Dahlke and published by . This book was released on 1973 with total page 51 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of Several Low Aspect Ratio Stabilizer Fins at Mach Numbers from 0.8 to 1.3 by : J. M. Whoric
Download or read book Aerodynamic Characteristics of Several Low Aspect Ratio Stabilizer Fins at Mach Numbers from 0.8 to 1.3 written by J. M. Whoric and published by . This book was released on 1972 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Fin-flare Combinations on the Aerodynamic Characteristics of a Body at Mach Numbers 1.61 and 2.20 by : Clyde Hayes
Download or read book Effect of Fin-flare Combinations on the Aerodynamic Characteristics of a Body at Mach Numbers 1.61 and 2.20 written by Clyde Hayes and published by . This book was released on 1965 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of Multiple Fins at Supersonic Mach Numbers by : Klaus O. Opalka
Download or read book Aerodynamic Characteristics of Multiple Fins at Supersonic Mach Numbers written by Klaus O. Opalka and published by . This book was released on 1969 with total page 74 pages. Available in PDF, EPUB and Kindle. Book excerpt: Selected test data are presented which show the aerodynamic properties of multiple fins, mounted on the tail section of slender bodies of revolution, as a function of the fin geometry at Mach numbers 1.75, 2.50, 3.50 and 4.50. Other parameters which alter the flow field past the fins such as the length of the forebody, the shape of the nose and the location of canard fins are also considered. (Author).
Book Synopsis Static Aerodynamic Stability Characteristics of a Body of Revolution with Wraparound Fins at Mach Numbers from 1.6 to 2.86 by : John E. Vaughn
Download or read book Static Aerodynamic Stability Characteristics of a Body of Revolution with Wraparound Fins at Mach Numbers from 1.6 to 2.86 written by John E. Vaughn and published by . This book was released on 1972 with total page 322 pages. Available in PDF, EPUB and Kindle. Book excerpt: Experimental aerodynamic investigations were conducted in the NASA Langley Unitary Plan wind tunnel for several wraparound fins with straight and with swept leading edge mounted on bodies of revolution. Mach number ranged from 1.6 to 2.86 while angle of attack was varied from -6 degrees to 6 degrees at 0 degrees sideslip angle. Six component aerodynamic force and moment data were recorded on the complete missile configuration while simultaneously recording the aerodynamic normal force and bending moments acting on each fin. The results of these tests are presented herein in plotted form. The number designation given the test is UPWT 980.
