Transonic aerodynamic characteristics of two hypersonic cruise configurations
Transonic aerodynamic characteristics of two hypersonic cruise configurations
Langhans, R. A.↗
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Subsonic Aerodynamic Characteristics of a Large-Scale 1.075-Pressure-Ratio Tip-Turbine Cruise-Fan Propulsion System at Angle of Attack
Wind tunnel tests of subsonic aerodynamic characteristics of large scale tip turbine cruise fan with 1.075 pressure ratio at angle of attack
Capone, Francis J.↗
Subsonic Performance Characteristics of a Large-Scale 1.075-Pressure-Ratio Tip-Turbine Cruise-Fan Propulsion System
Performance of turbine driven V/STOL cruise fan propulsion system at subsonic Mach numbers
Capone, F. J.↗
Flight and wind tunnel investigation of installation effects on supersonic cruise exhaust nozzles at transonic speeds.
Location effect of power plants on aft-mounted supersonic cruise exhaust nozzles at transonic speeds in flight and wind tunnel
Blaha, B. J.↗
Analytical heat transfer investigation of insulated liquid methane wing tanks for supersonic cruise aircraft
Heat transfer study of insulated liquid methane wing tank boiloff for supersonic cruise aircraft
Pleban, E. J.↗
Substantiation data for hypersonic cruise vehicle wing structure evaluation - Volume 1, sections 1-10
Trajectory, load, aerodynamic heating, materials, structural, and thermal analyses for hypersonic cruise vehicle wings
Davis, G. W.↗
Hypersonic cruise vehicle wing structure evaluation - Volume 2, sections 11-22
Structure size, weight, flutter, fatigue, creep, and heat shield analyses for hypersonic cruise vehicle wing
Davis, G. W.↗
Hypersonic cruise vehicle wing structure evaluation - Volume 3, sections 23-27
Cost, performance, reliability, interaction, and structural element analyses for hypersonic cruise vehicle wings
Davis, G. W.↗
Low-speed static stability and control characteristics of two small-scale, hypersonic cruise configurations
Low-speed static stability and control characteristics of two small-scale, hypersonic cruise vehicles
Freeman, D. C., Jr.↗
Solutions of two heat-transfer problems with application to hypersonic cruise aircraft
Heat transfer problem solutions with application to hypersonic cruise aircraft
Ardema, M. D.↗
A 90 degree sector development of a short length combustor for a supersonic cruise turbofan engine Interim report, Jun. 1968 - Mar. 1970
Short length combustor and diffuser configuration for supersonic cruise turbofan engine
Clements, T. R.↗
Subsonic cruise mode - An intact abort concept
Subsonic cruise mode for intact abort during ascent phase of space shuttle vehicles
Blanciak, A.↗
Flight investigation of the roll requirements for transport airplanes in cruising flight
Flight investigation of roll requirements for transport airplanes in cruising flight
Holleman, E. C.↗
Tests of a full-scale annular ram-induction combustor for a Mach 3 cruise turbojet engine
Full-scale annular ram-induction combustor tests for Mach 3 cruise turbojet engine
Perkins, P. J.↗
Effects of variable turbine area on subsonic cruise performance of turbojets designed for supersonic application
Effects of variable turbine area on subsonic cruise performance of turbojets designed for supersonic application
Keith, A. L., Jr.↗
Effects of wing elevation, incidence, and camber on the aerodynamic characteristics of a representative hypersonic cruise configuration at Mach numbers from 0.65 to 10.70
Wing elevation, incidence, and chamber effects on aerodynamic characteristics of representative hypersonic cruise configuration at Mach numbers from 0.65 to 10.70
Axelson, J. A.↗
Flying qualities of a large, supersonic aircraft in cruise and landing approach
XB-70 aircraft flight tests in cruise and landing approach to evaluate handling qualities criteria
Berry, D. T.↗
Optimal transition from entry to cruising flight
Optimal angle of attack transition trajectories for space shuttle from atmospheric entry to cruising flight for conventional airport landing
Stengel, R. F.↗