Explore Books on
research vehicles
1-24 of 28 Books
Numerical simulation of the flow about the F-18 HARV at high angle of attack
Numerical simulation of the flow about the F-18 HARV at high angle of attack
By Scott M. Murman
Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack
Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack
By Kenneth W. Iliff
Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring
Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring
By Kenneth W. Iliff
High-Alpha Research Vehicle (HARV) longitudinal controller
High-Alpha Research Vehicle (HARV) longitudinal controller
By Aaron J. Ostroff
Redesign of a variable-gain output feedback longitudinal controller flown on the High-Alpha Research Vehicle
Redesign of a variable-gain output feedback longitudinal controller flown on the High-Alpha Research Vehicle
By Aaron J. Ostroff
Spin-tunnel investigation of a 1/28-scale model of the NASA F-18 High Alpha Research Vehicle (HARV) with and without vertical tails
Spin-tunnel investigation of a 1/28-scale model of the NASA F-18 High Alpha Research Vehicle (HARV) with and without vertical tails
By Charles Michael Fremaux
Determining the accuracy of aerodynamic model parameters estimated from flight test data
Determining the accuracy of aerodynamic model parameters estimated from flight test data
By Eugene A. Morelli
Installed F/A-18 inlet flow calculations at 30 degrees angle-of-attack, a comparative study
Installed F/A-18 inlet flow calculations at 30 degrees angle-of-attack, a comparative study
By C. Frederic Smith
Performance validation of the ANSER control laws for the F-18 HARV
Performance validation of the ANSER control laws for the F-18 HARV
By Michael D. Messina
Computational analysis of forebody tangential slot blowing on the high alpha research vehicle
Computational analysis of forebody tangential slot blowing on the high alpha research vehicle
By Ken Gee
HARV ANSER flight test data retrieval and processing procedures
HARV ANSER flight test data retrieval and processing procedures
By Jessie C. Yeager
Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0 ̊to 70 ̊
Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0 ̊to 70 ̊
By Scott C. Asbury
Validation of the F-18 high alpha research vehicle flight control and avionics systems modifications
Validation of the F-18 high alpha research vehicle flight control and avionics systems modifications
By Vince Chacon
Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft
Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft
By
F/A-18A inlet flow characteristics during maneuvers with rapidly changing angle of attack
F/A-18A inlet flow characteristics during maneuvers with rapidly changing angle of attack
By Andrew J. Yuhas
High-alpha handling qualities flight research on the NASA F/A-18 High Alpha Research Vehicle
High-alpha handling qualities flight research on the NASA F/A-18 High Alpha Research Vehicle
By
The effects of pressure sensor acoustics on airdata derived from a high-angle-of-attack flush airdata sensing (HI-FADS) system
The effects of pressure sensor acoustics on airdata derived from a high-angle-of-attack flush airdata sensing (HI-FADS) system
By Stephen A. Whitmore
Singular perturbation analysis of AOTV-related trajectory optimization problems
Singular perturbation analysis of AOTV-related trajectory optimization problems
By Anthony J. Calise
Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0
Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0
By Ira J. Walker
Aircraft ground vibration testing at the NASA Dryden Flight Research Facility, 1993
Aircraft ground vibration testing at the NASA Dryden Flight Research Facility, 1993
By M. W. Kehoe
Fifty years of flight research
Fifty years of flight research
By David F. Fisher
Advances in experiment design for high performance aircraft
Advances in experiment design for high performance aircraft
By Engene A. Morelli