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EFFECTS OF AN IN-FLIGHT THRUST REVERSER ON THE STABILITY AND CONTROL CHARACTERISTICS OF A SINGLE-ENGINE FIGHTER AIRPLANE MODEL [NASA TN D-6886]

By: Mercer, C. E.

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BookSeries: National Aeronautics and Space Administration ; NASA Technical Note. Publisher: Washington, D.C. National Aeronautics and Space Administration 1972Description: 236p.Subject(s): Airplane model

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Item type	Current location	Collection	Call number	Vol info	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)		NASA TN D 6880-89	Not for loan		TR012230

Total holds: 0

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Previous	EXPERIMENTAL INVESTIGATION OF THE VISUAL FIELD DEPENDENCY IN THE ERECT AND SUPINE POSITIONS [NASA TN D-6883]	COMPARISON OF EXACT AND APPROXIMATE EVALUATIONS OF THE SINGLE-SCATTERING INTEGRAL IN NUCLEON-DEUTERON ELASTIC SCATTERING [NASA TN D-6884]	NUMERICAL SOLUTIONS OF SEVERAL REFLECTED SHOCK-WAVE FLOW FIELDS WITH NONEQUILIBRIUM CHEMICAL REACTIONS [NASA TN D-6885]	EFFECTS OF AN IN-FLIGHT THRUST REVERSER ON THE STABILITY AND CONTROL CHARACTERISTICS OF A SINGLE-ENGINE FIGHTER AIRPLANE MODEL [NASA TN D-6886]	ADHESION AND TRANSFER OF POLYTETRAFLUOROETHYLENE TO TUNGSTEN STUDIED BY FIELD ION MICROSCOPY [NASA TN D-6887]	RELATIONS AMONG PURE-TONE SOUND STIMULI NEURAL ACTIVITY AND THE LOUDNESS SENSATION [NASA TN D-6889]	9/1/2 foot diameter master and mirror.[NASA CR-103] [Bound contains NASA CR-101-103]	Next

Bound vol. contains NASA TN D 6880-89

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