Laminar, Transitional, and Turbulent Heating on Mid Lift-to-Drag Ratio Entry Vehicles-Reference-Cited by-同舟云学术

Laminar, Transitional, and Turbulent Heating on Mid Lift-to-Drag Ratio Entry Vehicles

Published:2013-09 Issue:5 Volume:50 Page:937-949
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Hollis Brian R.¹,Hollingsworth Kevin E.²

Affiliation:

1. Aerothermodynamics Branch, NASA Langley Research Center, Hampton, Virginia 23681

2. Supersonic/Hypersonic Test Branch, Aerospace Computing, Inc., Hampton, Virginia 23681

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A32458

Reference19 articles.

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3. Dwyer CiancioloA. D.DavisJ. L.ShidnerJ. D.PowellR. W. “Entry, Descent and Landing Systems Analysis: Exploration Class Simulation Overview and Results,” AIAA Paper 2010-7970, Aug. 2010.

4. ZangT. A.Dwyer CiancioloA. M.KinneyD. J.HowardA. R.ChenG. T.IvanovM. C.SostaricR. R.WesthelleC. H. “Overview of the NASA Entry, Descent and Landing Analysis Study,” AIAA Paper 2010-8649, Sept. 2010.

5. LockwoodM. K.EdquistK. T.StarrB. R.HollisB. R.HrindaG. A.BaileyR. W.HallJ. L.SpilkerT. R.NocaM. A.O'KongoN.HawR. J.JustusC. G.DuvallA. L.KellerV. W.MasciarelliJ. P.HoffmanD. A.ReaJ. R.WesthelleC. H.GravesC. A.TakashimaN.OlejniczakJ.ChenY. K.WrightM. J.LaubB.PrabhuD.DykeR. E.PrabhuR. K. “Aerocapture System Analysis for a Neptune Mission,” NASA TM-2006-214300, April 2006.

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