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NACA Research Memorandums
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An experimental study of five annular air inlet configurations at subsonic and transonic speeds
Free Flight Investigation at Transonic Speeds of the Power-on Characteristics Including Some Effects of Sonic Propulsive Jets of a Four Engine Delta Wing Configuration
Altitude chamber evaluation of an aircraft liquid hydrogen fuel system used with a turbojet engine
Design and performance of flight-type liquid-hydrogen heat exchanger
Design and Performance of Fuel Control for Aircraft Hydrogen Fuel System
Flight Investigation of a Liquid Hydrogen Fuel System
An experimental investigation of the unsteady lift induced on a wing in the downwash field of an oscillating canard control surface
Investigation of some wake vortex characteristics of an inclined ogive-cylinder body at Mach number 1.98
Investigation of Equilibrium Temperatures and Average Laminar Heat-Transfer Coefficients for the Front Half of Swept Circular Cylinders at a Mach Number of 6.9
Preliminary performance data of several tail-pipe-cascade-type model thrust reversers
Theoretical Investigation of Laminar Heat Transfer on Yawed Infinite Cylinders in Supersonic Flow and a Comparison With Experimental Data
Experimental investigation of a transonic compressor rotor with a 1.5-inch chord length and an aspect ratio of 3.0 2: blade-element performance
Tests of Aerodynamically Heated Multiweb Wing Structures in a Free Jet at Mach Number 2: Two Aluminum-Alloy Models of 20-Inch Chord With 0.064- and 0.081-Inch-Thick Skin
A preliminary investigation of static-pressure changes associated with combustion of aluminum borohydride in a supersonic wind tunnel
Performance of Inconel 550 Turbine Blades in a Turbojet Engine and Effects of Different Forging Temperatures and Heat Treatments
Flight Measurements of the Lateral Response Characteristics of the Convair XF-92A Delta-Wing Airplane
Performance of a short combustor at high altitudes using hydrogen fuel
Aircraft-Fuel-Tank Design for Liquid Hydrogen
Experimental investigation of methods of improving diffuser-exit total-pressure profiles for side-inlet model at Mach number 3.05
Drag Near Zero Lift of a 1/7-Scale Model of the Convair B-58 External Store as Measured in Free Flight Between Mach Numbers of 0.8 and 2.45
Investigation of impulse-type supersonic compressor with hub-tip ratio of 0.6 and turning to axial direction 2: stage performance with three different sets of stators
Experimental study of shock-positioning method of ram-jet-engine control
Static Longitudinal and Lateral Stability and Control Characteristics of an Airplane Configuration Having a Wing of Trapezoidal Plan Form With Various Tail Airfoil Sections and Tail Arrangements at a Mach Number of 6.86
A method for evaluating the loads and controllability aspects of the pitch-up problem
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