1-24 of 31 Books
Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code
Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code
By Wendy B. Lessard
Acoustic treatment design scaling methods
Acoustic treatment design scaling methods
By R. E. Kraft
Computer-aided light sheet flow visualization using photogrammetry
Computer-aided light sheet flow visualization using photogrammetry
By Kathryn Stacy
Low-order nonlinear dynamic model of IC engine-variable pitch propeller system for general aviation aircraft
Low-order nonlinear dynamic model of IC engine-variable pitch propeller system for general aviation aircraft
By Jacques C. Richard
Electromagnetic on-aircraft antenna radiation in the presence of composite plates
Electromagnetic on-aircraft antenna radiation in the presence of composite plates
By S. H-T Kan
Integrated Advanced Microwave Sounding Unit-A (AMSU-A), performance verification report, METSAT Phase Locked Oscillator assembly, P/N 1348360-1, S/N's F07 and F08
Integrated Advanced Microwave Sounding Unit-A (AMSU-A), performance verification report, METSAT Phase Locked Oscillator assembly, P/N 1348360-1, S/N's F07 and F08
By D. Pines
Structural dynamic model obtained from flight use with piloted simulation and handling qualities analysis
Structural dynamic model obtained from flight use with piloted simulation and handling qualities analysis
By Bruce G. Powers
High speed civil transport aircraft simulation
High speed civil transport aircraft simulation
By Robert A. Sotack
User's manual for interactive LINEAR, a FORTRAN program to derive linear aircraft models
User's manual for interactive LINEAR, a FORTRAN program to derive linear aircraft models
By Robert F. Antoniewicz
Development and implementation of software for visualizing and editing multidimensional flight simulation input data
Development and implementation of software for visualizing and editing multidimensional flight simulation input data
By Todd Michael Whelan
Effects of yaw and pitch motion on model attitude measurements
Effects of yaw and pitch motion on model attitude measurements
By Ping Tcheng
Controls design with crossfeeds for hovering rotcract using quantitative feedback theory
Controls design with crossfeeds for hovering rotcract using quantitative feedback theory
By Daniel J. Biezad
Controls design with crossfeeds for hovering rotorcraft using quantitative feedback theory
Controls design with crossfeeds for hovering rotorcraft using quantitative feedback theory
By Daniel J. Biezad
Acoustic and aerodynamic study of a pusher-propeller aircraft model
Acoustic and aerodynamic study of a pusher-propeller aircraft model
By Paul T. Soderman
Nonlinear axisymmetric and three-dimensional vorticity dynamics in a swirling jet model
Nonlinear axisymmetric and three-dimensional vorticity dynamics in a swirling jet model
By J. E. Martin
Generic airplane model concept and four specific models developed for use in piloted simulation studies
Generic airplane model concept and four specific models developed for use in piloted simulation studies
By Keith D. Hoffler
Simplified aerodynamic and structural modeling for oblique all-wing aircraft--phase 2: structures
Simplified aerodynamic and structural modeling for oblique all-wing aircraft--phase 2: structures
By Ilan Kroo
Measurements of pressures on the tail and aft fuselage of an airplane model during rotary motions at spin attitudes
Measurements of pressures on the tail and aft fuselage of an airplane model during rotary motions at spin attitudes
By James S. Bowman
NASA Dryden Flow Visualization Facility
NASA Dryden Flow Visualization Facility
By John H. Del Frate
Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane
Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane
By Dennis O. Allison
Activity tracking for pilot error detection from flight data
Activity tracking for pilot error detection from flight data
By Todd J. Callantine
A Modified lifted line theory for wing-propeller interference
A Modified lifted line theory for wing-propeller interference
By R. K. Prabhu
Numerical stability and control analysis towards falling-leaf prediction capabilities of splitflow for two generic high-performance aircraft models
Numerical stability and control analysis towards falling-leaf prediction capabilities of splitflow for two generic high-performance aircraft models
By Eric F. Charlton
A verification procedure for MSC/NASTRAN finite element models
A verification procedure for MSC/NASTRAN finite element models
By Alan E. Stockwell