DESIGN OF THE UNIVERSITY OF TENNESSEE HIGH-ENTHALPY TUNNEL

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Bibliographische Detailangaben
Veröffentlicht in:	AIAA SciTech Forum and Exposition (2021 : Online) Ground testing
1. Verfasser:	Byrd, Andrew J. (VerfasserIn)
Weitere Verfasser:	Baccarella, Damiano (VerfasserIn)
Format:	UnknownFormat
Sprache:	eng
Veröffentlicht:	2021
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SOME FUNDAMENTALS OF AEROPROPULSION FORCE ACCOUNTING	2021	Beale, David K.
DESIGN OF THE UNIVERSITY OF TENNESSEE HIGH-ENTHALPY TUNNEL	2021	Byrd, Andrew J.
DESIGN AND CHARACTERIZATION OF MACH 5 FLOW FOR HIGHLY TURBULENT HYPERSONIC TEST FACILITY	2021	Thornton, Mason R.
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DEVELOPMENT OF A DIRECT-CONNECT TESTING CAPABILITY IN THE HYPERTERP SHOCK TUNNEL	2021	Pee, Xiu Yi
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LIFT INTERFERENCE EFFECTS EVALUATION FOR POWERED MODELS IN CLOSED-WALL LOW-SPEED WIND TUNNELS	2021	Philipsen, Iwan
MODEL PREPARATION AREAS FOR PROPULSION AIRFRAME INTEGRATION TESTING AT THE NASA LANGLEY RESEARCH CENTER	2021	Jones, Gregory S.
UPWIND BUILDINGS EFFECTS ON TEST SECTION PERFORMANCE OF THE NFAC 80-BY 120-FOOT WIND TUNNEL	2021	Wagner, Lauren
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