NDLI: Supersonic aerodynamic characteristics associated with variations in the geometry of the forward portion of irregular planform wings. [based on wind tunnel tests of space shuttle orbiter configuration

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Supersonic aerodynamic characteristics associated with variations in the geometry of the forward portion of irregular planform wings. [based on wind tunnel tests of space shuttle orbiter configuration

Content Provider	NASA Technical Reports Server (NTRS)
Author	Stone, D. R. Spencer Jr., B.
Copyright Year	1973
Description	The experimental longitudinal and lateral-directional stability characteristics of a Langley conceptual space shuttle orbiter design have been obtained for a series of inboard planform fillets in a unitary plan wind tunnel. Fillet sweep angles up to 78 deg were investigated while holding the spanwise intersection of the fillet and wing constant. The data were obtained at Mach numbers of 2.36 to 4.63 and at Reynolds numbers (depending on Mach number) of 1.5 million to 2.5 million per foot. The angle of attack was varied from about minus 2 deg to 44 deg at 0 deg and 3 deg of sideslip.
File Size	12023279
Page Count	170
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19740004403
Archival Resource Key	ark:/13960/t2n639m5n
Language	English
Publisher Date	1973-10-01
Access Restriction	Open
Subject Keyword	Space Vehicles Aerodynamic Configurations Supersonic Speed Body-wing Configurations Wing Planforms Wind Tunnel Stability Tests Lateral Stability Space Shuttle Orbiters Longitudinal Stability Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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