Life Cycle Cost Modeling of High-Speed Commercial Aircraft: Final Review - Executive Summary
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 - Key Findings Detailed
Life Cycle Cost Modeling of High-speed Commercial Aircraft - Final Report
LTN Inlets and Nozzles Branch Overview; NASA GE - Methods Development Review
Life Cycle Cost Modeling of High-Speed Commercial Aircraft: Final Review - Executive Summary
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
Overview of Commercial High-Speed Market Studies and NASA’s Hypersonic Technology Project
Studies Relating to the Attainment of High Lift-Drag Ratios at Hypersonic Speeds
HYPERSONIC APPROXIMATION OF THE MINIMUM SEMIAPEX ANGLE GIVING SUBSONIC FLOW BEHIND AN ATTACHED SHOCK
State-of-the-ART Study for High-Speed Deceleration and Stabilization Devices Final Report
Hypersonic aerodynamic performance of minimum-wave-drag bodies
Transonic Aerodynamic Characteristics of Two Hypersonic Cruise Configurations
Design of the Phoenix Missile Hypersonic Testbed (PMHT)
Supersonic Investigation of Two Dimensional Hypersonic Exhaust Nozzles
Lift-to-drag ratios of slender wings at hypersonic speeds
Maximum lift-to-drag ratios of a slender, flat-top, hypersonic bodies, part 1
Chief Engineer's View of the NASA X-43A Scramjet Flight Test
New Air-Launched Small Missile (ALSM) Flight Testbed for Hypersonic Systems
RADIATIVE HEATING OF VEHICLES ENTERING THE EARTH'S ATMOSPHERE
Entropy Wake Behind a Sphere in Hypersonic Flight
Lift-TO-Drag Ratios of Slender Wings at Hypersonic Speeds
Two-dimensional approach to the maximum lift- to-drag ratio of a slender, flat-top, hypersonic wing
One-dimensional approach to the maximum lift- to-drag ratio of a slender, flat-top, hypersonic wing
Maximum lift-to-drag ratio of a slender wing at hypersonic speeds.
Flight Experiment Verification of Shuttle Boundary Layer Transition Prediction Tool
Maximum Lift-TO-Drag Ratios of a Slender, Flat-Top, Hypersonic Bodies, Part 1
Free-flight investigations of subliming ablators and transpiration cooling at hypersonic velocities