Sage Journals: Discover world-class research

Abstract

In the frame of the European Space Agency (ESA) Intermediate eXperimental Vehicle (IXV) project, ESA is coordinating a series of technical assistance activities aimed at verifying and supporting the IXV industrial design and development process. The technical assistance is operated by the Italian Space Agency, by means of the technical support of the Italian Aerospace Research Centre. One of the purposes of the activity is to develop an independent capability for the assessment and verification of the industrial results with respect to the aerothermodynamic characterization of the IXV vehicle. To this aim, CIRA have developed an independent aerothermodynamic database, intended as a tool generating in output the time histories of local quantities for each point of the IXV vehicle surface and for each trajectory, together with an uncertainties model. The whole procedure followed for the definition of the numerical tool and the main results achieved will be presented in this article.

Keywords

Aerothermodynamics re-entry IXV

Get full access to this article

View all access options for this article.

References

Rufolo

Roncioni

Marini

. Experimental and numerical aerodynamic data integration and aerodatabase development for the PRORA-USV1 reusable vehicle. 14th AIAA/AHI space planes and hypersonic systems and technologies conference. 6–9 November 2006

Canberra, Australia

Paper no. 2006-8031.

Rufolo

Roncioni

Marini

. Post flight aerodynamic analysis of the experimental vehicle PRORA USV 1. 15th AIAA international space planes and hypersonic systems and technologies conference. 28 April to 1 May, 2008

Dayton, OH

Paper no. 2008-2661.

Roncioni

Rufolo

Marini

. CFD rebuilding of USV-DTFT1 vehicle in-flight experiment. 59th international astronautical congress. 29 September to 3 October, 2008

Glasgow, Scotland, UK

Paper no. IAC-08-D2.6.02.

Roncioni

Ranuzzi

Marini

. CFD aerothermodynamic characterization of the IXV hypersonic vehicle. 7th European symposium on aerothermodynamics of space vehicles. 9–12 May 2011

Bruges, Belgium

Paper no. 2205059.

Walpot L. Development and application of a hypersonic ﬂow solver. PhD Thesis, T.U. Delft University, 2002.

Ranuzzi

Borreca

. CLAE Project. H3NS: code development and validation. Report no. CIRA-CF-06-1017, September 2006.

Park C. A review of reaction rates in high temperature air. AIAA Paper 89-1740, June 1989.

Millikan

Whit

. Systematic of vibrational relaxation. J Chem Phys 1963; 39(12): 3209–3213.

Park C. Validation of multi-temperature nozzle flow code NOZNT. AIAA Paper 93-2862, 1993.

10.

Yun

Mason

. A collision integrals for the transport properties of dissociating air at high temperatures. Phys Fluid 1962; 5(4): 380–386.

11.

Kee

Warnatz

Miller

. A Fortran computer code package for the evaluation of gas-phase viscosities, conductivities and diffusion coefficients. Sandia Rept. SAND83-8209. March 1983.

12.

Di Benedetto

. Definition and development of the ATDB tool surface interpolator. Report no. CIRA-CF-10-0631, April 2010.

13.

Schneider

. Effect of roughness on hypersonic boundary-layer transition. AIAA Paper 2007-0305 2007.

14.

NGL Team. Aerothermodynamics (ATD) wind tunnel testing (WTT). Report no. IXV-NGL-RPT-0028, 2008.

15.

Paris

. Aerothermodynamic WTT Report–Long-Shot. Report no. IXV-VKI-DF-001, 2008.

16.

Di Benedetto

. Definition of the IXV transition database. Report no. CIRA-CF-10-1113, October 2010.

17.

Reda

. Review and synthesis of roughness-dominated transition correlations for reentry applications. J Spacecraft Rocket 2002; 39(2): 161–167.

18.

Liechty DS, Berry SA, Hollis BR, et al. Comparison of methods for determining boundary layer edge conditions for transition correlations. AIAA Paper 2003–3590, 2003.

19.

Berry

Horvath

. Discrete roughness transition for hypersonic flight vehicles. J Spacecraft Rocket 2008; 45(2): 216–226.

20.

Horvath

Berry

Merski

. Hypersonic boundary/shear layer for blunt to slender configurations-A NASA langley experimental perspective. In: RTO AVT Lecture Series. RTO-MP-AVT-111, 2004.

21.

Arnal

Délery

. Laminar turbulent transition and shock wave/boundary layer interaction. In: RTO AVT Lecture Series. RTO-EN-AVT-116, 2004.

22.

Marini

. T1-98 transitional hyperboloid flare problem. In: First eastern- western high speed flow field database workshop, Kyoto, Japan, 1998.

23.

Anderson

. Hypersonic and high temperature gas dynamics, New York: McGraw-Hill Book Company, 1989.

24.

Ericsson

. Effect of nose bluntness and cone angle on slender-vehicle transition. AIAA J 1988; 26(10): 1168–1174.

25.

Blottner

. Finite difference method of solution of the boundary layer equations. AIAA J 1970; 8(2): 193–205.

26.

Kang

Jones

Dunn

. Theoretical and measured electron-density distributions at high altitudes. AIAA J 1973; 11(2): 141–149.

27.

Mareschi

. IXV Phase C2/D aerothermodynamic database. Report no. IXV-TASI-TNT-0024, 2011.

28.

GNC and flight management analysis report file. Report no. GNC011 – IXV-SDG-RPT-0102, Issue 1.2, 2011.

European Space Agency intermediate experimental vehicle: Development of an independent aerothermodynamic database tool

Abstract

Keywords

Get full access to this article

References