Flight and wind-tunnel comparisons of the inlet/airframe interaction of the F-15 airplane

by Lannie D. Webb

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
Published: Pages: 32 Downloads: 642
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Subjects:

  • Wind tunnels.,
  • Eagle (Jet fighter plane)

Edition Notes

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.

Full text of "DTIC ADA Aerodynamic Engine/Airframe Integration for High Performance Aircraft and Missiles (L'Integration Aerodynamique des Moteurs et des Cellules dans les Avions et les Missiles a Hautes Performances)" See other formats. Full text of "DTIC ADP Problems Associated with the Aerodynamic Design of Missile Shapes" See other formats PROBLEMS ASSOCIATED WITH THE AERODYNAMIC DESIGN OF MISSILE SHAPES Oi rp c: Jack N.

Nielsen Nielsen Engineering ^ Research, Inc. Mountain View, CAAbstract “"The purpose of the paper is to discuss ^^ /anous trends in the design of.

Tradeoffs in Jet Inlet Design: A Historical Perspective. intake wind-tunnel and flight tests were performed gives an overview of both inlet and nozzle integration for the F and FAuthor: Andras Sobester. An experimental investigation of flow control for supersonic inlets the flight and maneuver envelope of the airplane are reviewed.

in the entire wind tunnel. Comparisons are made with Author: Neil Titchener. Wind-tunnel tests used a percent-scale F inlet/airframe model. Flight and wind-tunnel pressure coefficients showed good agreement in most cases.

Correlation of interaction effects caused by changes in cowl angle, angle-of-attack, and Mach number are presented. Corrosion phenomena in sodium-potassium coolant resulting from solute interaction in multicomponent solution. NASA Astrophysics Data System (ADS) Krasin, V. P.; Soyustova, S.

A REVIEW OF CIVIL AERONAUTICS RESEARCH AND DEVELOPMENT HEARING BEFORE THE YF–16, YF–17, F–15, and EA–6B, just to name a few. Historically, flight tests were the only reliable source to find solutions to the problem. For example, the F/A–18E endured one and a half years of developmental flight-testing and evaluation of over Flight Testing and Simulation of an F Airplane Using Throttles for Flight Control.

6 7 5 4 NASA TM, H, NASAIAA 8 Paper Presented at the AIAA Flight Test Conference, Hilton Head, South Carolina, August 24 10 13 11 12 9.