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Nozzles -- Testing

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Filed under: Nozzles -- Testing

Static performance of nonaxisymmetric nozzles with yaw thrust-vectoring vanes (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), by Mary L. Mason, Bobby L. Berrier, and Langley Research Center (page images at HathiTrust)
Investigations of a flow field surrounding circular-arc boattail nozzles at subsonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by William Kelly Abeyounis, Lawrence E. Putnam, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
Pocketing mechanics of SRM nozzle liner (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), by V. Verderaime and George C. Marshall Space Flight Center (page images at HathiTrust)
Static investigation of circular-to-rectangular transition ducts for high-aspect-ratio nonaxisymmetric nozzles (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), by James R. Burley, John R. Carlson, Linda S. Bangert, and Langley Research Center (page images at HathiTrust)
Performance and durability of improved air-atomizing splash-cone fuel nozzles (National Aeronautics and Space Administration ;, 1974), by Robert D. Ingebo, Carl T. Norgren, and Lewis Research Center (page images at HathiTrust)
Effects of nozzle exit location and shape on propulsion-induced aerodynamic characteristics due to vectoring twin nozzles at Mach numbers from 0.4 ̥to 1.2 (U.S. National Aeronautics and Space Administration ;, 1976), by Francis J. Capone and Langley Research Center (page images at HathiTrust)
NASA TN D-4750 (National Aeronautics and Space Administration ;, 1968), by Kenneth Sutton, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
NASA TN D-5901 (National Aeronautics and Space Administration :, 1970), by Charles G. Miller, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Experiments upon the discharge of water through small fire hose and nozzles (1911), by Edward Oswald Korsmo and Alonzo Beda Neininger (page images at HathiTrust; US access only)
Root knots on fruit trees and vines ; A new nozzle tester (Agricultural Experiment Station, 1892), by C. W. Woodworth (page images at HathiTrust)

Filed under: Nozzles -- Testing -- Performance

NASA TN D-4592 (National Aeronautics and Space Administration ;, 1968), by Nelson L. Sanger, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)

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 supplies

Modifications to the nozzle test chamber to extend nozzle static-test capability (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by J. Wayne Keyes and Langley Research Center (page images at HathiTrust)

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)

Filed under: Spray nozzles -- Testing

High-pressure combustor exhaust emissions with improved air-atomizing and conventional pressure-atomizing fuel nozzles (National Aeronautics and Space Administration ;, 1973), by Robert D. Ingebo, Carl T. Norgren, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
A test of spray nozzles (University of the State of Missouri, College of Agriculture and Mechanic Arts, Agricultural Experiment Station, 1900), by N. O. Booth (page images at HathiTrust)

Filed under: Supersonic 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)
NASA TN D-5393 (National Aeronautics and Space Administration ;, 1969), by Bobbly Lee Berrier, Frederick H. Wood, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)

Filed under: Nozzles -- Fluid dynamics -- Testing

Performance of a composite solid propellant at simulated high altitudes (National Aeronautics and Space Administration, 1959), by Carl C. Ciepluch and Langley Research Center (page images at HathiTrust)

Filed under: Rockets (Aeronautics) -- Nozzles -- Testing

Experimental thrust performance of a high-area-ratio rocket nozzle (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), by Albert J. Pavli, Tamara A. Smith, Kenneth J. Kacynski, and Lewis Research Center (page images at HathiTrust)
Comparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m² (350 psia) (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), by Tamara A. Smith, Albert J. Pavli, Lewis Research Center, and Kenneth J. Kacynski (page images at HathiTrust)
Experimental evaluation of heat transfer on a 1030:1 area ratio rocket nozzle (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), by Kenneth J. Kacynski, Tamara A. Smith, Albert J. Pavli, and Lewis Research Center (page images at HathiTrust)
Supersonic investigation of nozzle hinge moments of a modified Saturn C-1 model with and without jet flow (National Aeronautics and Space Administration, 1963), by Nickolai Charczenko, Jerry L. Lowery, and Langley Research Center (page images at HathiTrust)
Performance of a variable divergent-shroud ejector nozzle designed for flight mach numbers up to 3.0 (National Aeronautics and Space Administration, 1961), by Andrew J. Stofan, James R. Mihaloew, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Comparison of rocket performance using exhaust diffuser and conventional techniques for altitude simulation (National Aeronautics and Space Administration, 1959), by Joseph N. Sivo, Daniel J. Peters, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Rocket-nozzle testing and evaluation (Columbus, Ohio : Battelle Memorial Institute, Defense Metals Information Center, 1960., 1960), by E. W. Ungar and Defense Metals Information Center (U.S.) (page images at HathiTrust)

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