Cover Image

A new theory for rapid calculation of the ground pattern of the incident sound intensity produced by a maneuvering jet airplane/

Main Author:	Barger, Raymond L.
Corporate Authors:	United States National Aeronautics and Space Administration Scientific and Technical Information Branch, Langley Research Center, United States. National Aeronautics and Space Administration., Scientific and Technical Information Branch
Format:	Book
Language:	English
Published:	Washington, D.C.: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980
Series:	NASA technical paper 1733
Subjects:	Jet planes > Noise

Similar Items

Mean velocity, turbulence intensity, and scale in a subsonic turbulent jet impinging normal to a large flat plate/
by: Boldman, Donald R.
Published: (1977)

Comparison of jet mach number decay data with a correlation and jet spreading contours for a large variety of nozzles/
by: Groesbeck, Donald E.
Published: (1977)

Application of second-order turbulent modeling to the prediction of radiated aerodynamic sound/
by: Bilanin, Alan J.
Published: (1978)

Interaction of a turbulent-jet noise source with transverse modes in a rectangular duct/
by: Succi, George P.
Published: (1978)

Measurements and predictions of flyover and static noise of a TF30 afterburning turbofan engine/
by: Burcham, Frank W.
Published: (1978)

Cumulative annoyance due to multiple aircraft flyovers with differing peak noise levels/
by: Shepherd, Kevin P.
Published: (1981)

The effect of forward speed on J85 engine noise from suppressor nozzles as measured in the NASA-Ames 40- by 80-foot wind tunnel/
by: Atencio, Adolph
Published: (1977)

Acoustic and aerodynamic performance of a 6-foot-diameter fan for turbofan engines : design of facility and QF-1 fan /
Published: (1970)

Effect of slotted casing treatment with change in Reynolds number index on performance of a jet engine/
by: Moss, John E.
Published: (1977)

Velocity field of a round jet in a cross flow for various jet injection angles and velocity ratios/
by: Fearn, Richard L.
Published: (1979)

Jet aircraft power systems : principles and maintenance /
Published: (1950)

Toxicologic assessment of jet-propulsion fuel 8
Published: (2003)

The jet V/STOL Harrier an evolutionary revolution in tactical air power /
Published: (1978)

Minimum-fuel, three-dimensional flightpath guidance of transport jets/
by: Neuman, Frank
Published: (1984)

Flight effects on noise generated by the JT8D-17 engine in a quiet nacelle and a conventional nacelle as measured in the NASA-Ames 40-by 80-foot wind tunnel : Summary report /
by: Strout, Frank G.
Published: (1976)

Experimental evaluation of a spinning-mode acoustic-treatment design concept for aircraft inlets/
by: Heidelberg, Laurence J.
Published: (1980)

Aerodynamics in ground effect and predicted landing ground roll of a fighter configuration with a secondary-nozzle thrust reverser/
by: Banks, Daniel W.
Published: (1988)

Flight effects on noise generated by the JT8D engine with inverted primary/fan flow as measured in the NASA-Ames 40- by 80-foot wind tunnel/
by: Strout, Frank G.
Published: (1978)

A forebody design technique for highly integrated botton-mounted scramjets with application to a hypersonic research airplane/
by: Edwards, C. L. W.
Published: (1976)

Turbulence measurements in supersonic, shock-free jets by the optical crossed-beam method/
by: Fischer, M. J.
Published: (1970)

Propulsion and Energetics Panel Working Group 13 on Alternative jet engine fuels/ Working Group 13
Published: (1982)

The application of parameter estimation to flight measurements to obtain lateral-directional stability derivatives of an augmented jet-flap STOL airplane/
by: Stephenson, Jack D. 1922-
Published: (1983)

Computational and experimental assessment of jets in cross flow= Evaluation numerique et experimentale des jets dans des courants transversaux/
Published: (1993)

Effect of simulated in-flight thrust reversing on vertical-tail loads of F-18 and F-15 airplane models/
by: Bare, E. Ann
Published: (1981)

Civil jet aircraft design /
by: Jenkinson, Lloyd R.
Published: (1999)

Flight comparison of the transonic agility of the F-111A airplane and the F-111 supercritical wing airplane/
by: Friend, Edward L.
Published: (1978)

Static and wind tunnel near-field/far-field jet noise measurements from model scale single-flow baseline and suppressor nozzles
by: Jaeck, Carl L.
Published: (1977)

Simulator study of stall/post-stall characteristics of a fighter airplane with longitudinal static stability/
Published: (1979)

Use of constrained optimization in the conceptual design of a medium-range subsonic transport/
by: Sliwa, Steven M.
Published: (1980)

Flight and wind-tunnel comparisons of the inlet/airframe interaction of the F-15 airplane/
by: Webb, Lannie D.
Published: (1984)

Simulator study of the effectiveness of an automatic control system designed to improve the high-angle-of-attack characteristics of a fighter airplane/
by: Gilbert, William P.
Published: (1976)

Effect of port corner geometry on the internal performance of a rotating-vane-type thrust reverser/
by: Berrier, Bobby L.
Published: (1986)

Static internal performance of a nonaxisymmetric vaned thrust reverser with flow splay capability/
by: Bangert, Linda S.
Published: (1989)

Effect of thrust reverser operation on the lateral-directional characteristics of a three-surface F-15 model at transonic speeds/
by: Bare, E. Ann
Published: (1983)

Static internal performance characteristics of two thrust-reverser concepts for axisymmetric nozzles/
by: Leavitt, Laurence D.
Published: (1982)

Impact study on the use of JET A fuel in military aircraft during operatios in Europe : etude de l' impact de l' utilization du carburant JET A par les avions militaires lors des operations en Europe /
by: Batchelor, Graham
Published: (1997)

Northrop F-5 case study in aircraft design
Published: (1978)

Flight evaluation of a simplified gross thrust calculation technique using an F100 turbofan engine in an F-15 airplane/
by: Kurtenbach, Frank J.
Published: (1981)

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

Performance of twin-dimensional wedge nozzles including thrust vectoring and reversing effects at speeds up to Mach 2.20/
by: Capone, Francis J.
Published: (1977)

Cannot write session to /tmp/vufind_sessions/sess_mgm7g2g0tkq8471vla4fq0rrk0