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| 035 | ⊔ | ⊔ | ‡a(MiU)99187539731306381 |
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| 040 | ⊔ | ⊔ | ‡aTRAAL ‡beng ‡cTRAAL ‡dTRAAL |
| 049 | ⊔ | ⊔ | ‡aMAIN |
| 086 | 0 | ⊔ | ‡aD 301.45/46-2:79-3138 Volume 1 |
| 100 | 1 | ⊔ | ‡aKnight, Doyle D., ‡eauthor. |
| 245 | 1 | 0 | ‡aCalculation of high speed inlet flows using the Navier-Stokes equations. ‡nVolume 1, ‡pDescription of results / Doyle D. Knight. |
| 264 | ⊔ | 1 | ‡aWright-Patterson Air Force Base, Ohio : ‡bAir Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, ‡c1980. |
| 300 | ⊔ | ⊔ | ‡axiv, 97 pages : ‡billustrations ; ‡c28 cm. |
| 336 | ⊔ | ⊔ | ‡atext ‡btxt ‡2rdacontent |
| 337 | ⊔ | ⊔ | ‡aunmediated ‡bn ‡2rdamedia |
| 338 | ⊔ | ⊔ | ‡avolume ‡bnc ‡2rdacarrier |
| 490 | 0 | ⊔ | ‡aAir Force Flight Dynamics Laboratory. Technical report - Air Force Flight Dynamics Laboratory ; ‡vAFFDL-TR-79-3138 Volume 1 |
| 500 | ⊔ | ⊔ | ‡a"February 1980." |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographic references (pages 40-42) |
| 520 | ⊔ | ⊔ | ‡aA set of computer programs has been developed to calculate the flowfield in two-dimensional mixed-compression high speed inlets. The full mean compressible Navier-Stokes equations are utilized, with turbulence represented by an algebraic eddy viscosity model which incorporates a relaxation correction. A curvilinear body-oriented coordinate system is employed to allow handling of arbitrary inlet contours. Boundary layer bleed is incorporated. The numerical algorithm of MacCormack is employed to solve the Navier-Stokes equations. A variety of techniques are incorporated to improve code efficiency, including time-splitting of the finite-difference operators, automatic mesh-splitting, and a separate algorithm for the treatment of the viscous sublayer portion of the turbulent boundary layers. The numerical codes have been successfully applied to the calculation of a variety of flows including shock-boundary layer interaction on a flat plate (including both unseparated and separated cases), and three different simulated high speed inlet configurations. In all cases, good agreement was obtained with the experimental data. |
| 536 | ⊔ | ⊔ | ‡aReport supported by the Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, and performed by Department of Mechanical, Industrial and Aerospace Engineering, Rutgers Univserity, New Brunswick, New Jersey, under contract no. ‡bF33615-78-C-3008. |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aTurbulent boundary layer. |
| 650 | ⊔ | 0 | ‡aNavier-Stokes equations. |
| 650 | ⊔ | 0 | ‡aAirplanes ‡xRamjet engines ‡xAir intakes. |
| 710 | 2 | ⊔ | ‡aAir Force Flight Dynamics Laboratory (U.S.), ‡esponsor. |
| 710 | 2 | ⊔ | ‡aRutgers University. ‡bDepartment of Mechanical & Aerospace Engineering, ‡esponsor. |
| 730 | 0 | ⊔ | ‡aTechnical Report Archive & Image Library (TRAIL) |
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| CID | ⊔ | ⊔ | ‡a102855463 |
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