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Aerodynamic Characteristics Of A Supersonic Cruise Airplane Configuration At Mach Numbers Of 230 296 And 330
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Book Synopsis Aerodynamic Characteristics of a Supersonic Cruise Airplane Configuration at Mach Numbers of 2.30, 2.96, and 3.30 by : Barrett L. Shrout
Download or read book Aerodynamic Characteristics of a Supersonic Cruise Airplane Configuration at Mach Numbers of 2.30, 2.96, and 3.30 written by Barrett L. Shrout and published by . This book was released on 1979 with total page 146 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics at Mach Numbers from 0.60 to 1.16 of a Canard Configuration Designed for Supersonic Cruise Flight by :
Download or read book Aerodynamic Characteristics at Mach Numbers from 0.60 to 1.16 of a Canard Configuration Designed for Supersonic Cruise Flight written by and published by . This book was released on 1960 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Supersonic Aerodynamic Characteristics of a Low-Drag Aircraft Configuration Having an Arrow Wing of Aspect Ratio 1.86 and a Body of Fineness Ratio 20 by :
Download or read book Supersonic Aerodynamic Characteristics of a Low-Drag Aircraft Configuration Having an Arrow Wing of Aspect Ratio 1.86 and a Body of Fineness Ratio 20 written by and published by . This book was released on 1960 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt: A free-flight rocket-propelled-model investigation was conducted at Mach numbers of 1.2 to 1.9 to determine the longitudinal and lateral aero-dynamic characteristics of a low-drag aircraft configuration. The model consisted of an aspect-ratio -1.86 arrow wing with 67.5 deg. leading-edge sweep and NACA 65A004 airfoil section and a triangular vertical tail with 60 deg. sweep and NACA 65A003 section in combination with a body of fineness ratio 20. Aerodynamic data in pitch, yaw, and roll were obtained from transient motions induced by small pulse rockets firing at intervals in the pitch and yaw directions. From the results of this brief aerodynamic investigation, it is observed that very slender body shapes can provide increased volumetric capacity with little or no increase in zero-lift drag and that body fineness ratios of the order of 20 should be considered in the design of long-range supersonic aircraft. The zero-lift drag and the drag-due-to-lift parameter of the test configuration varied linearly with Mach number. The maximum lift-drag ratio was 7.0 at a Mach number of 1.25 and decreased slightly to a value of 6.6 at a Mach number of 1.81. The optimum lift coefficient, normal-force-curve slope, lateral-force-curve slope, static stability in pitch and yaw, time to damp to one-half amplitude in pitch and yaw, the sum of the rotary damping derivatives in pitch and also in yaw, and the static rolling derivatives all decreased with an increase in Mach number. Values of certain rolling derivatives were obtained by application of the least-squares method to the differential equation of rolling motion. A comparison of the experimental and calculated total rolling-moment-coefficient variation during transient oscillations of the model indicated good agreement when the damping-in-roll contribution was included with the static rolling-moment terms.
Book Synopsis Aerodynamic Characteristics of a Tailless Fixed-wing Supersonic Transport Configuration at Mach Number 2.20 by : Gerald V. Foster
Download or read book Aerodynamic Characteristics of a Tailless Fixed-wing Supersonic Transport Configuration at Mach Number 2.20 written by Gerald V. Foster and published by . This book was released on 1964 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics at Mach Numbers from 0.6 to 2.16 of Supersonic Cruise Fighter Configuration with a Design Mach Mumber of 1.8 by : Barrett L. Shrout
Download or read book Aerodynamic Characteristics at Mach Numbers from 0.6 to 2.16 of Supersonic Cruise Fighter Configuration with a Design Mach Mumber of 1.8 written by Barrett L. Shrout and published by . This book was released on 1977 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Surface Pressure Data for a Supersonic-cruise Airplane Configuration at Mach Numbers of 2.30, 2.96, and 3.30 by : Barrett L. Shrout
Download or read book Surface Pressure Data for a Supersonic-cruise Airplane Configuration at Mach Numbers of 2.30, 2.96, and 3.30 written by Barrett L. Shrout and published by . This book was released on 1979 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Supersonic Aerodynamic Characteristics of an Advanced F-16 Derivative Aircraft Configuration by : Mike C. Fox
Download or read book Supersonic Aerodynamic Characteristics of an Advanced F-16 Derivative Aircraft Configuration written by Mike C. Fox and published by . This book was released on 1993 with total page 130 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Aerodynamic Characteristics of a Supersonic Cruise Aircraft Research Model with the Engines Suspended Above the Wing by : Charles E. Mercer
Download or read book Transonic Aerodynamic Characteristics of a Supersonic Cruise Aircraft Research Model with the Engines Suspended Above the Wing written by Charles E. Mercer and published by . This book was released on 1979 with total page 204 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics at Mach Numbers from 2.5 to 3.5 of a Canard Bomber Configuration Designed for Supersonic Cruise Flight by : Melvin M. Carmel
Download or read book Aerodynamic Characteristics at Mach Numbers from 2.5 to 3.5 of a Canard Bomber Configuration Designed for Supersonic Cruise Flight written by Melvin M. Carmel and published by . This book was released on 1958 with total page 53 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Supersonic Aerodynamic Characteristics of a Low-drag Aircraft Configuration Having an Arrow Wing of Aspect Ratio 1.86 and a Body of Fineness Ratio 20 by : Warren Gillespie Jr.
Download or read book Supersonic Aerodynamic Characteristics of a Low-drag Aircraft Configuration Having an Arrow Wing of Aspect Ratio 1.86 and a Body of Fineness Ratio 20 written by Warren Gillespie Jr. and published by . This book was released on 1960 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics at Mach Numbers from 0.6 to 2.16 of a Supersonic Cruise Fighter Configuration with a Design Mach Number of 1.8 by : Barrett L. Shrout
Download or read book Aerodynamic Characteristics at Mach Numbers from 0.6 to 2.16 of a Supersonic Cruise Fighter Configuration with a Design Mach Number of 1.8 written by Barrett L. Shrout and published by . This book was released on 1977 with total page 77 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Aerodynamic Characteristics at Mach Numbers from 0.60 to 2.70 of Two Supersonic Cruise Fighter Configurations by : Samuel M. Dollyhigh
Download or read book Experimental Aerodynamic Characteristics at Mach Numbers from 0.60 to 2.70 of Two Supersonic Cruise Fighter Configurations written by Samuel M. Dollyhigh and published by . This book was released on 1979 with total page 187 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of Aerodynamic Characteristics at High Subsonic Speeds of Two Supersonic- Cruise Airplane Configurations Having Tail Surfaces Outboard of the Wing Tips by :
Download or read book Investigation of Aerodynamic Characteristics at High Subsonic Speeds of Two Supersonic- Cruise Airplane Configurations Having Tail Surfaces Outboard of the Wing Tips written by and published by . This book was released on 1960 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of a Fixed Arrow-wing Supersonic Cruise Aircraft at Mach Numbers of 2.30, 2.70, and 2.95 by : Odell A. Morris
Download or read book Aerodynamic Characteristics of a Fixed Arrow-wing Supersonic Cruise Aircraft at Mach Numbers of 2.30, 2.70, and 2.95 written by Odell A. Morris and published by . This book was released on 1978 with total page 204 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Sonic-boom Characteristics of Proposed Supersonic and Hypersonic Airplanes by : F. Edward McLean
Download or read book Sonic-boom Characteristics of Proposed Supersonic and Hypersonic Airplanes written by F. Edward McLean and published by . This book was released on 1966 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of a Hypersonic Cruise Aircraft Concept with Wing-mounted Propulsion Systems at Mach Numbers of 2.96, 3.96, and 4.63 by : Gregory D. Riebe
Download or read book Aerodynamic Characteristics of a Hypersonic Cruise Aircraft Concept with Wing-mounted Propulsion Systems at Mach Numbers of 2.96, 3.96, and 4.63 written by Gregory D. Riebe and published by . This book was released on 1981 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:
