Subsonic static and dynamic stability characteristics of a NASP configuration

Subsonic static and dynamic stability characteristics of a NASP configuration

Wind-tunnel tests of a National Aero-Space Plane configuration were conducted, and the model used was a LaRC designed blended body configuration. The Aerodynmaic Preliminary Analysis System damping predictions were good for the roll mode and only fair for the pitch and yaw modes.

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Veröffentlicht in:Journal of aircraft 1994-07, Vol.31 (4), p.879-885
Hauptverfasser: BOYDEN, R. P, DRESS, D. A, FOX, C. H, HUFFMAN, J. K, CRUZ, C. I
Format: Artikel
Sprache:eng
Schlagworte:
Aerodynamics
Aircraft
Applied fluid mechanics
Exact sciences and technology
Fluid dynamics
Fundamental areas of phenomenology (including applications)
Physics
Tests
Wind tunnels
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Beschreibung
Zusammenfassung:Wind-tunnel tests of a National Aero-Space Plane configuration were conducted, and the model used was a LaRC designed blended body configuration. The Aerodynmaic Preliminary Analysis System damping predictions were good for the roll mode and only fair for the pitch and yaw modes.
ISSN:0021-8669
1533-3868
DOI:10.2514/3.46574