Jet nozzles -- Testing -- StatisticsSee also what's at your library, or elsewhere.
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Filed under: Jet nozzles -- Testing -- Statistics- Static internal performance of a two-dimensional convergent-divergent nozzle with thrust vectoring (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), by E. Ann Bare, David E. Reubush, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Effect of empennage arrangement on single-engine nozzle/afterbody static pressures at transonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1987), by William P. Henderson, James R. Burley, and Langley Research Center (page images at HathiTrust)
- Aeropropulsive characteristics of canted twin pitch-vectoring nozzles at Mach 0.20 to 1.20 (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), by Francis J. Capone, Mary L. Mason, and Langley Research Center (page images at HathiTrust)
- Parametric experimental investigation of a scramjet nozzle at Mach 6 with freon and argon or air used for exhaust simulation (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), by James M. Cubbage, William J. Monta, and Langley Research Center (page images at HathiTrust)
- A static investigation of the thrust vectoring system of the F/A-18 high-alpha research vehicle (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Mary L. Mason, Scott C. Asbury, Francis J. Capone, and Langley Research Center (page images at HathiTrust)
- Static internal performance of convergent single-expansion-ramp nozzles with various combinations of internal geometric parameters (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), by E. Ann Bare and Francis J. Capone (page images at HathiTrust)
- Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), by George T. Carson, Francis J. Capone, and Langley Research Center (page images at HathiTrust)
Items below (if any) are from related and broader terms.
Filed under: Jet nozzles -- Testing- Effect of a trade between boattail angle and wedge size on the performance of a nonaxisymmetric wedge nozzle (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), by George T. Carson, James R. Burley, E. Ann Bare, and Langley Research Center (page images at HathiTrust)
- Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20 (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), by George T. Carson, Milton Lamb, and Langley Research Center (page images at HathiTrust)
- Static performance of an axisymmetric nozzle with post-exit vanes for multiaxis thrust vectoring (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), by Bobby L. Berrier and Langley Research Center (page images at HathiTrust)
- Internal performance of two nozzles utilizing gimbal concepts for thrust vectoring (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Bobby L. Berrier, John G. Taylor, and Langley Research Center (page images at HathiTrust)
- Hot-flow tests of a series of 10-percent-scale turbofan forced mixing nozzles (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1984), by Verlon L. Head, William H. Gerstenmaier, Louis A. Povinelli, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Static internal performance of ventral and rear nozzle concepts for short-takeoff and vertical-landing aircraft (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), by Richard J. Re, George T. Carson, and Langley Research Center (page images at HathiTrust)
- Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), by Robert J. Foley, Odis C. Pendergraft, and Langley Research Center (page images at HathiTrust)
- Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by Mary L. Mason, Bobby L. Berrier, and Langley Research Center (page images at HathiTrust)
- Static internal performance of a two-dimensional convergent nozzle with thrust-vectoring capability up to 60 ̊ (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by Laurence D. Leavitt and Langley Research Center (page images at HathiTrust)
- Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), by Mary L. Mason, James R. Burley, and Langley Research Center (page images at HathiTrust)
- Cold-flow performance of several variations of a ram-air-cooled plug nozzle for supersonic-cruise aircraft (National Aeronautics and Space Administration ;, 1974), by Douglas E. Harrington, David M. Straight, Stanley M. Nosek, and Lewis Research Center (page images at HathiTrust)
- Flight investigation of installation effects on a wedge nozzle installed on an underwing nacelle (National Aeronautics and Space Administration ;, 1975), by Albert L. Johns and Lewis Research Center (page images at HathiTrust)
- Internal performance of a hybrid axisymmetric/nonaxisymmetric convergent-divergent nozzle (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), by John G. Taylor and Langley Research Center (page images at HathiTrust)
- Acoustic tests of a 15.2-centimeter-diameter potential flow convergent nozzle (National Aeronautics and Space Administration ;, 1974), by Allen M. Karchmer, Robert Friedman, Robert G. Dorsch, and Lewis Research Center (page images at HathiTrust)
- Effect of several geometric parameters on the static internal performance of three nonaxisymmetric nozzle concepts (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by Bobby L. Berrier, Richard J. Re, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Thrust performance of isolated 36-chute suppressor plug nozzles with and without ejectors at Mach numbers from 0 to 0.45 (National Aeronautics and Space Administration ;, 1975), by Douglas E. Harrington, Stanley A. Skebe, James J. Schloemer, and Lewis Research Center (page images at HathiTrust)
- Static performance of a cruciform nozzle with multiaxis thrust-vectoring and reverse-thrust capabilities (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by David J. Wing, Scott C. Asbury, and Langley Research Center (page images at HathiTrust)
- Analysis and testing of two-dimensional slot nozzle ejectors with variable area mixing sections (National Aeronautics and Space Administration ;, 1973), by Gerald B. Gilbert, Philip G. Hill, Ames Research Center, and Dynatech R/D Company (page images at HathiTrust)
- Performance of an isolated two-dimensional variable-geometry wedge nozzle with translating shroud and collapsing wedge at speeds up to Mach 2.01 (National Aeronautics and Space Administration ;, 1975), by Donald L. Maiden and Langley Research Center (page images at HathiTrust)
- Noncavitating and cavitating performance of several low area ratio water jet pumps having throat lengths of 3.54 diameters (National Aeronautics and Space Administration ;, 1969), by Nelson L. Sanger, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
- Surface pressure distributions with a sonic jet normal to adjacent flat surfaces at Mach 2.92 to 6.4 (National Aeronautics and Space Administration, 1961), by Robert W. Cubbison, James J. Ward, Bernhard H. Anderson, and Lewis Research Center (page images at HathiTrust)
- Static and wind-on tests of an upper-surface-blown jet-flap nozzle arrangement for use on the Quiet Clean Shore-haul Experimental Engine (QCSEE) (National Aeronautics and Space Administration ;, 1977), by Arthur E. Phelps, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Filed under: Jet nozzles -- Testing -- Equipment and suppliesFiled under: Exhaust nozzles -- Testing- Aerodynamic and acoustic investigation of inverted velocity profile coannular exhaust nozzle models and development of aerodynamic and acoustic prediction procedures (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by Richard S. Larson, Bradley S. Stevens, Douglas P. Nelson, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- A preliminary assessment of the impact of 2-D exhaust-nozzle geometry on the cruise range of a hypersonic aircraft with top-mounted ramjet propulsion (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by Walter A. Vahl, John P. Weidner, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Filed under: Jet nozzles -- Effect of temperature on -- Testing
Filed under: Jet nozzles -- Statistics |