Flight and wind-tunnel comparisons of the inlet/airframe interaction of the F-15 airplane
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch, Publisher: For sale by the National Technical Information Service] in Washington, D.C, [Springfield, Va
Written in English
- Wind tunnels.,
- Eagle (Jet fighter plane)
|Statement||Lannie D. Webb, Dom Andriyich-Varda, and Stephen A. Whitmore.|
|Series||NASA technical paper -- 2374.|
|Contributions||Andriyich-Varda, Dom., Whitmore, Stephen A., United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.|
|The Physical Object|
|Pagination||32 p. :|
|Number of Pages||32|
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Flight and wind-tunnel comparisons of the inlet/airframe interaction of the F-15 airplane by Lannie D. Webb Download PDF EPUB FB2
Flight and wind-tunnel comparisons of the inlet/airframe interaction of the F airplane. Washington, D.C.: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va.
Scale Adaptive Simulations over a Supersonic Car. Authors; Authors and affiliations Varda, D., Whitmore, S.: Flight and Wind-tunnel Comparisons of the Inlet/Airframe Interaction of the F Airplane.
NASA Evans B., Hassan O., Morgan K. () Scale Adaptive Simulations over a Supersonic Car. In: Kuzmin A. (eds) Computational Fluid Author: Guillermo Araya, Ben Evans, Oubay Hassan, Kenneth Morgan. Preliminary flight and wind tunnel comparisons of the inlet/airframe interaction of the F airplane.
WEBB, S. WHITMORE and; R. JANSSEN; Amplification factors at transition on an unswept wing in free flight and on a swept wing in wind.
Webb, L.; Varda, D.; Whitmore, S. Flight and Wind-Tunnel Comparisons of the Inlet/Airframe Interaction of the F Airplane; Technical Paper ; NASA: Washington, DC, USA, Figure 1.
Mesh schematic (a); close-up of the near wall region (b); and iso-contours of turbulent kinetic energy from Menter SST (c) in the supersonic flat by: 3.
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