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SPEED
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Concepts for Multi-Speed Rotorcraft Drive System - Status of Design and Testing at NASA GRC
LTN Inlets and Nozzles Branch Overview; NASA GE - Methods Development Review
Acoustic Testing of a High-Tip-Speed Fan with Bypass-Duct Liners - Overview
Concepts for Multi-Speed Rotorcraft Drive System - Status of Design and Testing at NASA GRC
Life Cycle Cost Modeling of High-Speed Commercial Aircraft: Final Review - Key Findings Detailed
Life Cycle Cost Modeling of High-speed Commercial Aircraft - Final Report
Life Cycle Cost Modeling of High-Speed Commercial Aircraft: Final Review - MIDAS Development & Demo
Life Cycle Cost Modeling of High-Speed Commercial Aircraft: Final Review - Executive Summary
Approach Considerations in Aircraft with High-Lift Propeller Systems
The Factors that Determine the Minimum Speed of an Airplane
An Investigation of Airplane Landing Speeds
Life Cycle Cost Modeling of High-Speed Commercial Aircraft: Final Review - Key Findings Detailed
Life Cycle Cost Modeling of High-Speed Commercial Aircraft: Final Review - MIDAS Development & Demo
Life Cycle Cost Modeling of High-speed Commercial Aircraft - Final Report
Life Cycle Cost Modeling of High-Speed Commercial Aircraft: Final Review - Executive Summary
Transonic and Supersonic Flutter Trend Investigation of a Variable-sweep Wing
Overview of Commercial High-Speed Market Studies and NASA’s Hypersonic Technology Project
Flight experience with the Ogee wing at low speed
State-of-the-ART Study for High-Speed Deceleration and Stabilization Devices Final Report
Regionalization of MERRA-2 50-m Wind Speed over the United States for Energy Applications
Handling Qualities of Large Rotorcraft in Hover and Low Speed
An Analysis of the Gust-Induced Overspeed Trends of Helicopter Rotors
Evaluation of Unmanned Radar Installations
Aerodynamic Characteristics and Glide-Back Performance of Langley Glide-Back Booster
Summary of the Large Civil Tiltrotor (LCTR2) Engine Gearbox Study
The Effects of Aerodynamic Brakes upon the Speed Characteristics of Airplanes
Aerodynamic characteristics of a family of multistage missiles at a mach number of 6.0
Transonic and Supersonic Flutter Trend Investigation of a Variable-Sweep Wing
A Performance Application Study of a Jet-Flap Helicopter Rotor
High-speed Wind-tunnel Tests of Gun Openings in the Nose of the Fuselage of a 1/4-scale Model
Design Study of Propulsion and Drive Systems for the Large Civil TiltRotor (LCTR2) Rotorcraft