Body of revolution
Resource Information
The concept Body of revolution represents the subject, aboutness, idea or notion of resources found in University of Oklahoma Libraries.
The Resource
Body of revolution
Resource Information
The concept Body of revolution represents the subject, aboutness, idea or notion of resources found in University of Oklahoma Libraries.
- Label
- Body of revolution
- Authority link
- http://id.worldcat.org/fast/00835380
- Source
- fast
29 Items that share the Concept Body of revolution
Context
Context of Body of revolutionSubject of
- A Method for determining the aerodynamic characteristics of two- and three-dimensional shapes at hypersonic speeds
- A comparison of the experimental subsonic pressure distributions about several bodies of revolution with pressure distributions computed by means of the linearized theory
- A pressure-distribution investigation of a fineness-ratio-12.2 parabolic body of revolution (NACA RM-10) at M : 1.59 and angles of attack up to 36°
- Aerodynamic-heating data obtained from free-flight tests between Mach numbers of 1 and 5
- An analysis of the applicability of the hypersonic similarity law to the study of flow about bodies of revolution at zero angle of attack
- An analysis of the pressure distribution measured on a body of revolution at transonic speeds in the slotted test section of the Langley 8-foot transonic tunnel
- Average skin-friction coefficients from boundary-layer measurements on an ogive-cylinder body in flight at supersonic speeds
- Average skin-friction drag coefficients from tank tests of a parabolic body of revolution (NACA RM-10)
- Calculation of compressible potential flow past slender bodies of revolution by an integral method
- Drag measurements at transonic speeds of two bodies of fineness ratio 9 with different locations of maximum body diameter
- Effect of spin on aerodynamic properties of bodies of revolution
- Effects of some external-store mounting arrangements and store shapes on the buffet and drag characteristics of wingless rocket-powered models at Mach numbers from 0.7 to 1.4
- Experimental investigation of temperature recovery factors on bodies of revolution at supersonic speeds
- Experimental investigation of the effects of support interference on the drag of bodies of revolution at a Mach number of 1.5
- Flight investigation at high-subsonic, transonic, and supersonic speeds to determine zero-lift drag of fin-stabilized bodies of revolution having fineness ratios of 12.5, 8.91, and 6.04 and varying positions of maximum diameter
- Flow over a slender body of revolution at supersonic velocities
- Free-flight measurements of aerodynamic heat transfer to Mach number 3.9 and of drag to Mach number 6.9 of a fin-stabilized cone-cylinder configuration
- Investigation at supersonic speeds of the variation with Reynolds number and Mach number of the total, base, and skin-friction drag of seven boattail bodies of revolution designed for minimum wave drag
- Investigation of the drag of blunt-nosed bodies of revolution in free flight at Mach numbers from 0.6 to 2.3
- Investigation of the variation with Reynolds number of the base, wave, and skin-friction drag of a parabolic body of revolution (NACA RM-10) at Mach numbers of 1.62, 1.93, and 2.41 in the Langley 9-inch supersonic tunnel
- Investigations at supersonic speeds of the base pressure on bodies of revolution with and without sweptback stabilizing fins
- Preliminary investigation of the effects of heat transfer on boundary-layer transition on a parabolic body of revolution (NACA RM-10) at a Mach number of 1.61
- Preliminary surveys of the three dimensional boundary layer on a yawed, spinning body of revolution
- Pressure distribution and some effects of viscosity on slender inclined bodies of revolution
- Pressure measurements on a body of revolution in the Langley 16-foot transonic tunnel and a comparison with free-fall data
- The effects of a small jet of air exhausting from the nose of a body of revolution in supersonic flow
- The flow past a straight- and a swept-wing-body combination and their equivalent bodies of revolution at Mach numbers near 1.0
- Theoretical investigation at subsonic speeds of the flow ahead of a slender inclined parabolic-arc body of revolution and correlation with experimental data obtained at low speeds
- Theoretical investigation of transonic similarity for bodies of revolution
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<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.libraries.ou.edu/resource/ZN92Sc3u5OI/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.libraries.ou.edu/resource/ZN92Sc3u5OI/">Body of revolution</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.libraries.ou.edu/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.libraries.ou.edu/">University of Oklahoma Libraries</a></span></span></span></span></div>
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<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.libraries.ou.edu/resource/ZN92Sc3u5OI/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.libraries.ou.edu/resource/ZN92Sc3u5OI/">Body of revolution</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.libraries.ou.edu/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.libraries.ou.edu/">University of Oklahoma Libraries</a></span></span></span></span></div>
