Review on Analysis & Modeling of Dynamic Stability Characteristics of Atmospheric Entry Vehicles

Authors

  • Atiqa Bibi
  • Adnan Maqsood Research Centre for Modeling & Simulation, National University of Sciences & Technology
  • Tiauw Hiong Go

DOI:

https://doi.org/10.24949/njes.v7i1.121

Abstract

Atmospheric entry is a critical phase for mission that seeks to return astronauts or scientific payloads back to Earth or explore the surface of a planet with an appreciable atmosphere. This paper presents a review of the comprehensive investigations on the dynamic stability of blunt body atmospheric entry vehicle.  As blunt vehicle enters a planetary atmosphere, the aerodynamic moments acting upon it can result in unstable pitching motions and divergence of oscillation amplitude. Typically, these instabilities are found in the low or mid supersonic regime of the trajectory just prior to parachute deployment. A discussion on the underlying phenomena of dynamic stability is followed by effect of geometric and design parameters on stability. Numerical  and analytical procedures used for modeling of the complex phenomena are also examined.

Author Biography

Adnan Maqsood, Research Centre for Modeling & Simulation, National University of Sciences & Technology

Dr. Adnan Maqsood is working as Assistant Professor at Research Center for Modeling and Simulation, National University of Sciences and Technology (NUST), Pakistan, since 2012. He received his Bachelor degree in Aerospace Engineering from NUST, Pakistan in 2005 and PhD from Nanyang Technological University (NTU), Singapore in January 2012. Dr. Adnan Maqsood has done significant research work and published several top quality international conferences and journal papers.  He has been often invited as a reviewer for a number of conferences, journals and book reviews. The current research interests of Dr. Adnan Maqsood are associated with:

  • Applied & Computational Aerodynamics
  • Unmanned Air Vehicle (UAV) Systems
  • Flight Dynamics and Control
  • Nonlinear Dynamics
  • Wind Energy

References

NCA okays Nuclear Power Prog 2050, Space Prog 2040. The News International Directorate for Science & Technology 2011 22 January 2015].

FAA. Returning from Space: Re-entry. Available from: https://www.faa.gov/other_visit/aviation_industry/designees_delegations/designee_types/ame/media/Section%20III.4.1.7%20Returning%20from%20Space.pdf.

Abilleira, F. and J. Shidner, Entry, Descent, and Landing Communications for the 2011 MARS Science Laboratory, in 23rd International Symposium on Space Flight Dynamics. 2012: Pasadena, CA.

Kazemba, C.D., R.D. Braun, I.G. Clark, and M. Schoenenberger, Survey of Blunt Body Dynamic Stability in Supersonic Flow, in AIAA Atmospheric Flight Mechanics Conference. 2012, AIAA: Minnesota, USA.

Kazemba, C.D., R.D. Braun, I.G. Clark, and M. Schoenenberger, Survey of Blunt Body Dynamic Stability in Supersonic Flow, in AIAA Atmospheric Flight Mechanics Conference. 2012: Minnesota, USA.

Jaremenko, I.M., Wakes Their Structure and Influence Upon Aerodynamic Decelerators. 1967. NASA CR-74.

Teramoto, S., K. Hiraki, and K. Fujii, Numerical analysis of dynamic stability of a reentry capsule at transonic speeds. American Institute of Aeronautics and Astronautics, 1998.

Donald A. Buell, N.S.J., An Experimental and Analytical Investigation of The Dynamics of Two Blunt Bodies at Subsonic Speeds. NASA TECHNICAL MEMORANDUM 1959(X - 18).

Ericsson, L. and J. Reding, Reentry capsule dynamics. Atmospheric Flight Mechanics Conference, 1970.

Chapman, G., R. Mitcheltree, and W. Hathaway, Transonic and low supersonic static and dynamic aerodynamic characteristics of the Stardust sample return capsule. 37th AIAA Aerospace Sciences Meeting and Exhibit, 1999(AIAA 99-1021).

Jaffe, P. and R.H. Prislin, Angle-of-attack motion of a spinning entry vehicle. Journal of Spacecraft and Rockets, 1969. 6(1): p. pg. 93-96.

John D. Bird, D.E.R., Jr, Stability of Ballistic Reentry Bodies. NACA RM L-58, 1958.

Fletcher, H.S., Damping in Pitch and Static Stability of a Group of Blunt Bodies from M=0.6 to 0.95. NASA TM X-194, 1959(TM X-194).

Wolhart, H.S.F.a.W.D., Damping In Pitch and Static Stability of Supersonic Impact Nose Cones, Short Blunt Subsonic Impact Nose Cones, and Manned Reentry Capsules at Mach Numbers From 1.93 to 3.05. 1960(NASA TM X-347).

Smith, B., Oscillation of Supersonic Inflatable Aerodynamic Decelerators at Mars. Masters Project, Georgia Institute of Technology, 2010.

D. B. Owens, V.V.A., Overview of Orion Crew Module and Launch Abort Vehicle Dynamic Stability 29th AIAA Applied Aerodynamics Conference, 2011.

A. L. Ramsey, G.T.C., A study of Reynolds number effects on supersonic flow over blunt bodies. 38th Aerospace Sciences Meeting & Exhibit, 2000(AIAA 2000-1010 ).

G. T. Chapman, L.A.Y., Dynamics of Planetary Probes: Design and Testing Issues. 1998(AIAA 1998-0797).

Krumins, M.V., Drag and Stability of Mars Probe/Lander Shapes. Journal of Spacecraft and Rockets, 1967. vol. 4(no. 8): p. pg. 1052-1057.

Hayes, W.D., Probstein, R. F., Hypersonic Flow Theory I. 1960, Academic Press, New York.

Busemann, A., Handworterbuck der Naturwissenschaften,Fliissigkeits und Gasbewegung. 1933, Gustav Fisher, Jena. p. pg.244-279.

Seiff, A., Secondary Flow Fields Embedded in Hypersonic ShockLayers. , 1962(NASA TN D-1304).

Ericsson, L.E., Unsteady Aerodynamics of an Ablating Flared Body of Revolution Including Effects of Entropy Gradient. AIAA Journal, 1968. Vol. 6: p. pg.2395-2401.

Ericsson, L.E., Generalized Unsteady Embedded Newtonian Flow. Journal of Spacecraft and Rockets, 1975. vol. 12(no. 12): p. pg. 718-726.

Tong, B.G.a.H., W. H., Unsteady Embedded Newton-Busemann Flow Theory. Journal of Spacecraft and Rockets, 1986 Vol. 23(no.2): p. pg. 129-135

Murman, S.M., Reduced-Frequency Approach for Calculating Dynamic Derivatives. AIAA Journal, 2007 vol. 45(no. 6): p. pg. 1161-1168.

S. M. Murman, M.J.A., Dynamic Analysis of Atmospheric-Entry Probes and Capsules. 45th AIAA Aerospace Sciences Meeting, 2007. AIAA 2007-0074: p. pg.1-18.

E.Stern, V.G., G. Chandler, Estimation of Dynamic Stability Coefficients for Aerodynamic Decelerators Using CFD, in AIAA Applied Aerodynamics Conference, New Orleans, LA,. 2012.

Downloads

Published

2015-07-10

Issue

Section

Engineering Sciences