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Francis J Capone

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WingsAeropropulsive characteristics of twin nonaxisymmetric vectoring nozzles installed with forward swept and aft-swept wingsFrancis J. Capone

Aeropropulsive characteristics of twin nonaxisymmetric vectoring nozzles installed with forward swept and aft-swept wings

Francis J. Capone · National Aeronautics and Space Administration, Scientific and Technical Information Branch

258 sayfa · 1981

Aerodynamics / Airplanes / Wings

Thrust reversersPerformance of twin-dimensional wedge nozzles including thrust vectoring and reversing effects at speeds up to Mach 2.20Francis J Capone

Performance of twin-dimensional wedge nozzles including thrust vectoring and reversing effects at speeds up to Mach 2.20

Francis J Capone · for sale by the National Technical Information Service

188 sayfa · 1977

Jet nozzles / Jet planes / Thrust reversers

AerodynamicsParametric investigation of single-expansion-ramp nozzles at Mach numbers from 0.60 to 1.20Francis J. Capone

Parametric investigation of single-expansion-ramp nozzles at Mach numbers from 0.60 to 1.20

Francis J. Capone · National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program

Sayfa sayısı yok · 1992

Nozzles / Aerodynamics

Wind tunnel calibrationThe NASA Langley 16-Foot Transonic TunnelFrancis J. Capone

The NASA Langley 16-Foot Transonic Tunnel

Francis J. Capone · Langley Research Center

197 sayfa · 1995

Transonic wind tunnels / Wind tunnel calibration

Transonic planesEffects of varying podded nacelle-nozzle installations on transonic aeropropulsive characteristics of a supersonic fighter aircraftFrancis J Capone

Effects of varying podded nacelle-nozzle installations on transonic aeropropulsive characteristics of a supersonic fighter aircraft

Francis J Capone · National Aeronautics and Space Administration, Scientific and Technical Information Branch

334 sayfa · 1983

Airplanes / Canard Wings / Nacelles / Supersonic planes / Transonic planes

NozzlesStatis performance of five twin-engine nonaxisymmetric nozzles with vectoring and reversing capabilityFrancis J Capone

Statis performance of five twin-engine nonaxisymmetric nozzles with vectoring and reversing capability

Francis J Capone · for sale by the National Technical Information Service

63 sayfa · 1978

Nozzles

Fighter planesEffect of thrust vectoring and wing maneuver devices on transonic aeropropulsive characteristics of a supersonic fighter aircraftFrancis J Capone

Effect of thrust vectoring and wing maneuver devices on transonic aeropropulsive characteristics of a supersonic fighter aircraft

Francis J Capone · National Aeronautics and Space Administration, Scientific and Technical Information Branch

85 sayfa · 1983

Jet nozzles / Fighter planes

Fighter planesMultiaxis aircraft control power from thrust vectoring at high angles of attackFrancis J. Capone

Multiaxis aircraft control power from thrust vectoring at high angles of attack

Francis J. Capone · For sale by the National Technical Information Service

Sayfa sayısı yok · 1986

Thrust / Airplanes / Motors / Fighter planes

Jet nozzlesAeropulsive characteristics at Mach numbers up to 2.2 of axisymmetric and nonaxisymmetric nozzles installed on an F-18 modelFrancis J Capone

Aeropulsive characteristics at Mach numbers up to 2.2 of axisymmetric and nonaxisymmetric nozzles installed on an F-18 model

Francis J Capone · For sale by the National Technical Information Service]

77 sayfa · 1982

Jet nozzles

Short take-off and landing aircraftInterference effects of thrust reversing on horizontal tail effectiveness of a twin-engine fighter aircraft at Mach numbers from 0.15 to 0.9Francis J. Capone

Interference effects of thrust reversing on horizontal tail effectiveness of a twin-engine fighter aircraft at Mach numbers from 0.15 to 0.9

Francis J. Capone · For sale by the National Technical Information Service]

Sayfa sayısı yok · 1986

Fighter planes / Short take-off and landing aircraft

MotorsAeropropulsive characteristics of canted twin pitch-vectoring nozzles at Mach 0.20 to 1.20Francis J. Capone

Aeropropulsive characteristics of canted twin pitch-vectoring nozzles at Mach 0.20 to 1.20

Francis J. Capone · National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division

Sayfa sayısı yok · 1991

Thrust / Jet nozzles / Testing / Airplanes / Motors

Fighter aircraftAerodynamic characteristics of a supersonic fighter aircraft model at Mach 0.40 to 2.47Francis J. Capone

Aerodynamic characteristics of a supersonic fighter aircraft model at Mach 0.40 to 2.47

Francis J. Capone · National Aeronautics and Space Administration, Scientific and Technical Information Branch

Sayfa sayısı yok · 1986

Aerodynamic characteristics / Aerodynamics, Supersonic / Data bases / Databases / Fighter aircraft

Fighter planesInvestigation of Axisymmetric and nonaxisymmetric nozzels installed on a 0.10-scale F-18 protype airplane modelFrancis J Capone

Investigation of Axisymmetric and nonaxisymmetric nozzels installed on a 0.10-scale F-18 protype airplane model

Francis J Capone · For sale by the National Technical Information Service]

301 sayfa · 1980

Testing / Aerodynamics / Airplanes / Fighter planes

Drag (Aerodynamics)Effects of empennage surface location on aerodynamic characteristics of a twin-engine afterbody model with nonaxisymmetric nozzlesFrancis J. Capone

Effects of empennage surface location on aerodynamic characteristics of a twin-engine afterbody model with nonaxisymmetric nozzles

Francis J. Capone · National Aeronautics and Space Administration, Scientific and Technical Information Branch

Sayfa sayısı yok · 1985

Drag (Aerodynamics)

MotorsStatic internal performance of a single expansion ramp nozzle with multiaxis thrust vectoring capabilityFrancis J. Capone

Static internal performance of a single expansion ramp nozzle with multiaxis thrust vectoring capability

Francis J. Capone · National Technical Information Service, distributor]

Sayfa sayısı yok · 1993

Thrust / Jet nozzles / Airplanes / Motors

Fighter planesMultiaxis control power from thrust vectoring for a supersonic fighter aircraft model at Mach 0.20 to 2.47Francis J. Capone

Multiaxis control power from thrust vectoring for a supersonic fighter aircraft model at Mach 0.20 to 2.47

Francis J. Capone · National Aeronautics and Space Administration, Scientific and Technical Information Office

Sayfa sayısı yok · 1987

Thrust / Airplanes / Motors / Fighter planes