Cover Image

Investigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft /

Bibliographic Details
Main Authors:	Berrier, Bobby L. (Author), Re, Richard J. (Author)
Corporate Author:	Langley Research Center
Format:	Government Document eBook
Language:	English
Published:	[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.
Series:	NASA technical paper ; 1766.
Subjects:	Convergent-divergent nozzles. Mach number. Nozzle design. Performance tests. Pressure ratio.
Online Access:	https://purl.fdlp.gov/GPO/gpo71372

Similar Items

Transonic investigation of two-dimensional nozzles designed for supersonic cruise /
by: Capone, Francis J., et al.
Published: (2015)

Effects of sidewall geometry on the installed performance of nonaxisymmetric convergent-divergent exhaust nozzles /
by: Yetter, Jeffery A., et al.
Published: (1980)

Conceptual design for a dual-bell rocket nozzle system using a NASA F-15 airplane as the flight testbed /
by: Jones, Daniel S.
Published: (2014)

Effects of nozzle exit geometry and pressure ratio on plume shape for nozzles exhausting into quiescent air /
by: Scallion, W. I.
Published: (1991)

Near-exit pressure fluctuations in jets from circular and rectangular nozzles /
by: Zaman, K. B. M. Q. (Khairul B. M. Q.), et al.
Published: (2019)

Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf /
by: Lamb, Milton, et al.
Published: (1996)

Vacuum chamber pressure effects on thrust measurements of low Reynolds number nozzles /
Published: (1985)

Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20 /
by: Carson, George T., et al.
Published: (1988)

Exhaust nozzle plume effects on sonic boom test results for isolated nozzles /
by: Castner, Raymond S.
Published: (2011)

Exhaust nozzle plume and shock wave interaction /
by: Castner, Raymond S., et al.
Published: (2013)

Slot nozzle effects for reduced sonic boom on a generic supersonic wing section /
by: Castner, Raymond S.
Published: (2010)

A performance comparison of two small rocket nozzles /
by: Arrington, Lynn A., et al.
Published: (1996)

Calibration for thrust and airflow measurements in the CE-22 Advanced Nozzle Test Facility /
by: Werner, Roger A.
Published: (2010)

Acoustic measurements of rectangular nozzles with bevel /
by: Bridges, James E., 1943-
Published: (2012)

Comparison of numerically simulated and experimentally measured performance of a rotating detonation engine /
by: Paxson, Daniel E.
Published: (2015)

Noise from aft deck exhaust nozzles : differences in experimental embodiments /
by: Bridges, James E.
Published: (2014)

Methodology for three dimensional nozzle design /
by: Ferri, Aldo A., et al.
Published: (1974)

Exhaust environment measurements of a turbofan engine equipped with an afterburner and 2D nozzle /
by: Brase, L. O.
Published: (1990)

Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure /
by: Hussaini, M. Moin, et al.
Published: (1996)

Exit boundary layer data for a round convergent nozzle in support of numerical simulation efforts /
by: Zaman, K. B. M. Q. (Khairul B. M. Q.)
Published: (2019)

Analysis and design of optimized truncated scarfed nozzles subject to external flow effects /
by: Shyne, Rickey J.
Published: (1990)

Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet /
by: Ponton, Michael K., et al.
Published: (1999)

Internal thrust and pumping performance of an auxiliary inlet ejector nozzle with clamshell thrust reverser /
by: Mansour, Ali H., et al.
Published: (1969)

Separate flow nozzle test status meeting : proceedings of a conference held at and sponsored by NASA Glenn Research Center, Cleveland, Ohio, September 9-10, 1997 /
Published: (2000)

Computational simulations of convergent nozzles for the AIAA 1st Propulsion Aerodynamics Workshop /
by: Dippold, Vance
Published: (2014)

Exhaust nozzle plume effects on sonic boom test results for vectored nozzles /
by: Castner, Raymond S.
Published: (2012)

Flow processes in overexpanded chemical rocket nozzles.
by: Schmucker, Robert H.
Published: (1984)

Static internal performance of a two-dimensional convergent nozzle with thrust-vectoring capability up to 60 ̊ /
by: Leavitt, Laurence D.
Published: (1985)

Mach 5 electroformed nickel nozzle refurbishment : FNAS investigation of ultra-smooth surfaces /
by: Rood, Robert, et al.
Published: (1992)

Flow-field surveys for rectangular nozzles /
by: Zaman, K. B. M. Q. (Khairul B. M. Q.)
Published: (2012)

Converging-diverging nozzle thruster code for nuclear or chemical rocket performance computations /
by: Juhasz, Albert J.
Published: (2019)

Multidisciplinary approach to aerospike nozzle design /
by: Korte, J. J.
Published: (1997)

Measured pressure distributions inside nonaxisymmetric nozzles with partially deployed thrust reversers /
by: Green, Robert S.
Published: (1987)

Supersonic wind tunnel nozzles : a selected, annotated bibliography to aid in the development of quiet wind tunnel technology /
by: Wolf, Stephen W. D.
Published: (1990)

A survey of challenges in aerodynamic exhaust nozzle technology for aerospace propulsion applications /
by: Shyne, Rickey J.
Published: (2002)

A survey of challenges in aerodynamic exhaust nozzle technology for aerospace propulsion applications /
by: Shyne, Rickey J.
Published: (2002)

Operating characteristics of the multiple critical venturi system and secondary calibration nozzles used for weight-flow measurements in the Langley 16-foot transonic tunnel /
by: Berrier, Bobby L.
Published: (1985)

Trapped waves and screech tones with various rectangular nozzles /
by: Zaman, K. B. M. Q. (Khairul B. M. Q.), et al.
Published: (2021)

Experimental evaluation of a translating nozzle sidewall radial turbine /
by: Roelke, Richard J.
Published: (1987)

Shelf life extension for the lot AAE nozzle severance LSCs : final test report /
by: Cook, M.
Published: (1990)