Lift, Drag and Thrust Measurement in a Hypersonic Impulse Facility

Tuttle, S. L., Mee, D. J. and Simmons, J. M. (1994). Lift, Drag and Thrust Measurement in a Hypersonic Impulse Facility. In: Proceedings of the AIAA 18th Aerospace Ground Testing Conference. AIAA 18th Aerospace Ground Testing Conference, Colorado Springs, CO, (). 20-23 June, 1994.

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Author Tuttle, S. L.
Mee, D. J.
Simmons, J. M.
Title of paper Lift, Drag and Thrust Measurement in a Hypersonic Impulse Facility
Conference name AIAA 18th Aerospace Ground Testing Conference
Conference location Colorado Springs, CO
Conference dates 20-23 June, 1994
Proceedings title Proceedings of the AIAA 18th Aerospace Ground Testing Conference
Publication Year 1994
Sub-type Fully published paper
Language eng
Abstract/Summary This paper reports the extension of the stress wave force balance to the measurement of forces on models which are non-axisymmetric or which have non-axisymmetric load distributions. Recent results are presented which demonstrate the performance of the stress wave force balance for drag measurement, for three-component force measurement and preliminary results for thrust measurement on a two-dimensional scramjet nozzle. In all cases, the balances respond within a few hundred microseconds.
Subjects 290201 Aerodynamics
Keyword force measurement
stress wave force balance
scramjet
References Carbonaro, M. "Aerodynamic Force Measurements in the VK.I Longshoi Hypersonic Facility", in New Trends in Instrumentation for Hypersonic Research, (ed. A. Boutier). Kluwer, Dordrecht, pp 3 17-325, 1993. Jessen, C. Gmnig, H, "A Six Component Balance tor Short Duration Hypersonic facilities", in New Trends in Instrumentation for Hypersonic Research, (ed. A. Boutier), Kluwer, Dordrecht, pp 295-305, 1993. Naumann, K W, Ende, H, Mathieu, G, "Millisecond Aerodynamic Force Measurement Technique for High Enthalpy Test Facilities", in New Trends in Instrumentation for Hypersonic Research, (ed. A. Boutier), Kluwer, Dordrecht, pp 307-316, 1993. Sanderson, S.R., Simmons, J.M., Tuttle, S.L., "A Drag Measurement Technique for Free Piston Shock Tunnels", AIAA-91-0549, 29th Aerospace Sciences Meeting, Reno, Nevada, Jan. 7-10, 1991. Prost, R., Goutte, R., "Discrete Constrained Iterative Deconvolution Algorithms with Optimised Rate of Convergence", Signal Processing, 7, 209-230,1984. Sanderson, S.R., Simmons, J.M., "Drag Balance for Hypervelocity Impulse facilities", AIAA Journal, Vol. 29, No. 12, pp. 2185-2191, December 1991. Taylor, G.I. and Maccoll, J.W., "The Air Pressure on a Cone Moving at High Speed", Proc. Roy. Soc. (London), Ser. A, 139, pp 278-297, 1932. Mee, D.J., Daniel, W.J., Tuttle, S.L., Simmons, J.M., "Balances for the Measurement of Multiple Components of Force in flows of a Millisecond Duration", Proc. 19th International Symposium on Shock Waves, 26-30 July, Marseilles, France, 1993. Jones, D.J., "Tables of lnviscid Supersonic Flow about Circular Cones at Incidence, gamma = 1.4", AGARDograph 137, 1969. Mee, D.J., "Uncertainty Analysis of Conditions in the Test Section of the T4 Shock Tunnel", Research Report 4/93, Dept. of Mech. Eng., The University of Queensland, 1993. Simmons, J.M., Daniel, W.J., Mee, D.J., and Tuttle, S.L., "Force Measurement in Hypervelocity Impulse Facilities", in New Trends in Instrumentation for Hypersonic Research, (ed. A. Boutier), Kluwer, Dordrecht, pp 285-294. Schetz. J.A,, Billig, F.S., Favin, S., "Numerical Solutions of Scramjet Nozzle Flows", J. Propulsion, Vol. 3, No. 5, 1986.
Q-Index Code E1
Q-Index Status Provisional Code
Institutional Status Unknown
Additional Notes Paper number AIAA-94-2596

Document type: Conference Paper
Collection: School of Mechanical & Mining Engineering Publications
 
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Created: Tue, 03 Jan 2006, 10:00:00 EST by David J Mee on behalf of Library Corporate Services