#
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

## Context

Context of Body of revolution#### Subject 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>`