Download or read book Static Aerodynamic Characteristics of Three Rocket vehicle Configurations at Mach Numbers from 1 80 to 4 63 Including Some Effects of Fin Size Fin Cant and Auxiliary Rocket Motors written by Dennis E. Fuller and published by . This book was released on 1963 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Static Aerodynamic Characteristics of Three Rocket vehicle Configurations at Mach Numbers from 1 80 to 4 63 Including Some Effects of Fin Size Fin Cant and Auxiliary Rocket Motors written by Dennis E. Fuller and published by . This book was released on 1963 with total page 51 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Scientific and Technical Reports written by United States. National Aeronautics and Space Administration Scientific and Technical Information Division and published by . This book was released on 1964 with total page 260 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book A Selected Listing of NASA Scientific and Technical Reports for written by United States. National Aeronautics and Space Administration. Scientific and Technical Information Division and published by . This book was released on 1963 with total page 258 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Static Aerodynamic Characteristics of a Two stage and a Three stage Rocket Vehicle at Mach Numbers from 1 47 to 4 63 written by Clarence A. Brown and published by . This book was released on 1962 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Static Aerodynamic Characteristics of a Two stage and a Three stage Rocket Vehicle at Mach Numbers from 1 47 to 4 63 written by CLARENCE A. JR. BROWN and published by . This book was released on 1962 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was conducted in the Langley Unitary Plan wind tunnel to determine the effects of fin cant and size on the static aerodynamic characteristics of a 0.081-scale model of a three-stage and a two-stage Trailblazer II configuration. Tests were performed at Mach numbers from 1.47 to 4.63 and at a Reynolds number per foot of 3.0 x 10 to the 6th power. he angleof-attack range varied from approximately -5 to 5 degrees and angle of sideslip varied from approximately -4 to 4 degrees. All first-stage fins tested gave adequate static stability when the center-of-gravity travel of the flight model was taken into account. The presence of the auxiliary rocket motors in the lateral plane decreased the effectiveness of the fins in the pitch plane at the lower Mach number and increased the fin effectiveness at the higher Mach numbers. Removal of the auxiliary rocket motors from the first stage of the two-stage configuration reduced the axial force about 25% at the low Mach numbers and about 15% at the high Mach numbers. (Author).
Download or read book Static Aerodynamic Characteristics of a Three stage Rocket Vehicle Having Various Fin Configurations at Low Subsonic Mach Numbers and Angles of Attack Up to 28 written by Clarence A. Brown and published by . This book was released on 1963 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA SP written by and published by . This book was released on 1964 with total page 262 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book A Selected Listing of Nasa Scientific and Technical Reports for 1963 written by and published by . This book was released on 1964 with total page 254 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Static Aerodynamic Characteristics of a Three stage Rocket Vehicle Having Various Fin Configurations at Low Subsonic Mach Numbers and Angles of Attack Up to 28 Degrees written by Clarence A. Jr Brown and published by . This book was released on 1963 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Static Aerodynamic Characteristics of a Rocket Vehicle with Thick Wedge Fins and Sweptback Leading and Trailing Edges written by Joseph A. Yuska and published by . This book was released on 1966 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: The longitudinal static stability characteristics of three one-fifth scale models of the second stage of a sounding rocket were calculated and compared with the measured values at Mach numbers of 1.79 to 3.47. All three models had fins of trapezoidal planform with sweptback leading and trailing edges, small aspect ratio, and thick wedge sections, but differed in fin area and overall model length. Calculation of center of pressure and normal-force coefficient slope at zero normal force were in good agreement with experimental data.
Download or read book Static Stability Investigation of a Sounding rocket Vehicle at Mach Numbers from 1 50 to 4 63 written by C. Donald Babb and published by . This book was released on 1967 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aerodynamic Characteristics in Pitch of a 1 7 scale Model of a Two and Three stage Rocket Configuration at Mach Numbers of 0 4 to 4 63 written by William F. Hinson and published by . This book was released on 1969 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aerodynamic characteristics in pitch of scale model of two and three stage rocket configuration at Mach numbers of 0.4 to 4.63.
Download or read book Effects of Body and Fin Deflections on the Aerodynamic Characteristics in Pitch of a 0 065 scale Model of a Four stage Rocket Configuration at Mach Numbers of 1 41 and 1 82 written by Ross B. Robinson and published by . This book was released on 1959 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aerodynamic Characteristics from Mach 0 22 to 4 65 of a Two stage Rocket Vehicle Having an Unusual Nose Shape written by John T. Suttles and published by . This book was released on 1964 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Static Longitudinal Stability of a Rocket Vehicle Having a Rear facing Step Ahead of the Stabilizing Fins written by Robert J. Keynton and published by . This book was released on 1961 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: "Tests were conducted at Mach numbers of 3.96 and 4.65 in the Langley Unitary Plan wind tunnel to determine the static longitudinal stability characteristics of a fin-stabilized rocket-vehicle configuration which had a rearward facing step located upstream of the fins. Two fin sizes and planforms, a delta and a clipped delta, were tested. The angle of attack was varied from 6° to -6° and the Reynolds number based on model length was about 10 x 106. The configuration with the larger fins (clipped delta) had a center of pressure slightly rearward of and an initial normal-force-curve slope slightly higher than that of the configuration with the smaller fins (delta) as would be expected. Calculations of the stability parameters gave a slightly lower initial slope of the normal-force curve than measured data, probably because of boundary-layer separation ahead of the step. The calculated center of pressure agreed well with the measured data. Measured and calculated increments in the initial slope of the normal-force curve and in the center of pressure, due to changing fins, were in excellent agreement indicating that separated flow downstream of the step did not influence flow over the fins. This result was consistent with data from schlieren photographs."--P. 1.
Download or read book Aerodynamic Characteristics at Mach Numbers from 1 60 to 2 16 of a Blunt nose Missile Model Having a Triangular Cross Section and Fixed Triform Fins written by William J. Monta and published by . This book was released on 1971 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
