Thrust Control

84 books
Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0 deg to 70 degScott C. Asbury
⏱ 2h 53m

Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0 deg to 70 deg

Scott C. Asbury

1995173 pp.
A simulation evaluation of a four-engine jet transport using engine thrust modulation for flightpath controlUnknown Author

A simulation evaluation of a four-engine jet transport using engine thrust modulation for flightpath control

Unknown Author

1991No page data
Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0 ̊to 70 ̊Scott C. Asbury

Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0 ̊to 70 ̊

Scott C. Asbury

1995No page data
Design, analysis and control of large transports so that control of engine thrust can be used as a back-up of the primary flight controlsJan Roskam

Design, analysis and control of large transports so that control of engine thrust can be used as a back-up of the primary flight controls

Jan Roskam

1995No page data
Aeroservoelastic modeling and validation of a thrust-vectoring F/A-18 aircraftMartin J. Brenner

Aeroservoelastic modeling and validation of a thrust-vectoring F/A-18 aircraft

Martin J. Brenner

1996No page data
HARV ANSER flight test data retrieval and processing proceduresJessie C. Yeager

HARV ANSER flight test data retrieval and processing procedures

Jessie C. Yeager

1997No page data
Simulator evaluation of simplified propulsion-only emergency flight control systems on transport aircraftUnknown Author

Simulator evaluation of simplified propulsion-only emergency flight control systems on transport aircraft

Unknown Author

1999No page data
Evaluation of four advanced nozzle concepts for short takeoff and landing performanceP. Frank Quinto
⏱ 1h 35m

Evaluation of four advanced nozzle concepts for short takeoff and landing performance

P. Frank Quinto

199395 pp.
An experimental/modeling study of jet attachment during counterflow thrust vectoringPaul J. Strykowski

An experimental/modeling study of jet attachment during counterflow thrust vectoring

Paul J. Strykowski

1997No page data
Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction controlScott C. Asbury

Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control

Scott C. Asbury

1999No page data
Static internal performance of a nonaxisymmetric vaned thrust reverser with flow splay capabilityLinda S. Bangert

Static internal performance of a nonaxisymmetric vaned thrust reverser with flow splay capability

Linda S. Bangert

1989No page data
Integrated control using the SOFFT control structureNesim Halyo
⏱ 1h 32m

Integrated control using the SOFFT control structure

Nesim Halyo

199692 pp.
An analysis of cross-coupling of a multi component jet engine test stand using finite element modeling techniquesWilliam G. Schweikhard

An analysis of cross-coupling of a multi component jet engine test stand using finite element modeling techniques

William G. Schweikhard

1995No page data
A vehicle health monitoring system for the space shuttle reaction control system during reentryAnthony David Rosello

A vehicle health monitoring system for the space shuttle reaction control system during reentry

Anthony David Rosello

1995No page data
Development and flight test of an emergency flight control system using only engine thrust on an MD-11 transport airplaneUnknown Author

Development and flight test of an emergency flight control system using only engine thrust on an MD-11 transport airplane

Unknown Author

1997No page data
Hot gas ingestion test results of a two-poster vectored thrust concept with flow visualization in the NASA Lewis 9- x 15-foot low speed wind tunnelUnknown Author

Hot gas ingestion test results of a two-poster vectored thrust concept with flow visualization in the NASA Lewis 9- x 15-foot low speed wind tunnel

Unknown Author

1990No page data
Piloted evaluation of an integrated methodology for propulsion and airframe control designUnknown Author

Piloted evaluation of an integrated methodology for propulsion and airframe control design

Unknown Author

1994No page data
Application of an integrated methodology for propulsion and airframe control design to a STOVL aircraftSanjay Garg

Application of an integrated methodology for propulsion and airframe control design to a STOVL aircraft

Sanjay Garg

1994No page data
Development and flight test of an augmented thrust-only flight control system on an MD-11 transport airplaneUnknown Author

Development and flight test of an augmented thrust-only flight control system on an MD-11 transport airplane

Unknown Author

1996No page data
Effects of turbulence and delay in activating TIGER II after low altitute releaseRonald W. Greene
⏱ 20h 9m

Effects of turbulence and delay in activating TIGER II after low altitute release

Ronald W. Greene

19791209 pp.
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