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- Effects of Some Configuration Changes on Afterburner Combustion Performance
- Boundary-Layer-Transition and Heat-Transfer Measurements from Flight Tests of Blunt and Sharp 50 Degree Cones at Mach Numbers from 1.7 to 4.7
- An Investigation at Low Speed of the Spin Instability of Mortar-Shell Tails
- A Study of Injection Processes for 15-percent Fluorine-85- Percent Oxygen and Heptane in a 200-pound-thrust Rocket Engine
- On the minimization of airplane responses to random gusts
- Determination of surge and stall limits of an axial-flow turbojet engine for control applications
- The minimization of wave drag for wings and bodies with given base area or volume
- Investigation of combustion in 16-inch ram jet under simulated conditions of high altitude and high Mach number
- Flight and analytical methods for determining the coupled vibration response of tandem helicopters
- Effects of Inlet Modification and Rocket-Rack Extension on the Longitudinal Trim and Low-Lift Drag of the Douglas F5D-1 Airplane as Obtained with a 0.125-Scale Rocket-Boosted Model Between Mach Numbers of 0.81 and 1.64: TED No. NACA AD 399
- Near Noise Field of a Jet-Engine Exhaust
- Effects of Inlet Modification and Rocket-Rack Extension on the Longitudinal Trim and Low-Lift Drag of the Douglas F5D-1 Airplane as Obtained with a 0.125-Scale Rocket-Boosted Model between Mach Numbers of 0.81 and 1.64, TED No. NACA AD 399
- Determination of longitudinal stability and control characteristics from free-flight model tests with results at transonic speeds for three airplane configurations
- An investigation of single- and dual-rotation propellers at positive and negative thrust, and in combination with an NACA 1-series D-type cowling at Mach numbers up to 0.84
- Experimental and predicted longitudinal and lateral-directional response characteristics of a large flexible 35 degree swept-wing airplane at an altitude of 35,000 feet
- Determination of vortex paths by series expansion technique with application to cruciform wings
- Experimental investigation of effects of moderate sideslip on the flow fields near a 45 degree swept-wing-fuselage combination at low speed
- Summary of scale-model thrust-reverser investigation
- Relation of Turbojet and Ramjet Combustion Efficiency to Second-Order Reaction Kinetics and Fundamental Flame Speed
- Heat of Combustion of the Product Formed by the Reaction of Acetylene and Diborane (LFPL-CZ-3)
- Comparison of the Combustion Performance of Shell UMF, Grade C, MIL-F-5624C, Grade JP-5, Fuels in a Heavy-Duty XRJ47-W-9 Ram-Jet Engine
- Endurance Evaluation of Sintered, Porous, Strut-Supported Turbine Blades made by Federal-Mogul-Bower-Bearings, Incorporated, under Bureau of Aeronautics Contract NOas 55-124-C
- Two-dimensional airfoil characteristics of four NACA 6A-series airfoils at transonic Mach numbers up to 1.25
- Minimum wave drag for arbitrary arrangements of wings and bodies
- Seat Design for Crash Worthiness
- An analysis of the effects of aeroelasticity on static longitudinal stability and control of a swept-wing airplane
- On flow of electrically conducting fluids over a flat plate in the presence of a transverse magnetic field
- Some effects of bluntness on boundary-layer transition and heat transfer at supersonic speeds
- Three-dimensional transonic flow theory applied to slender wings and bodies
- Flight investigation of the effectiveness of an automatic aileron trim control device for personal airplanes
- A variational theorem for creep with applications to plates and columns
- On panel flutter and divergence of infinitely long unstiffened and ring-stiffened thin-walled circular cylinders
- Extended operation of turbojet engine with pentaborane
- Cloud-droplet ingestion in engine inlets with inlet velocity ratios of 1.0 and 0.7
- Effect of fuel variables on carbon formation in turbojet-engine combustors
- Investigation of two-stage air-cooled turbine suitable for flight at Mach number of 2.5 2: blade design
- Internal Performance of Several Divergent-Shroud Ejector Nozzles with High Divergence Angles
- Investigation of ejection release characteristics of bluff TX-28 and turnabout TX-28 stores from a 1/17-scale simulated bomb bay of the Republic F-105 airplane at Mach numbers of 1.39 and 1.98 : COORD. No. AF-222
- Investigation of ejection releases of an MB-1 rocket from a 0.04956-scaled model of the Convair F-106A airplane at several Mach numbers and simulated attitudes : COORD. No. AF-AM-57
- Investigation of ejection releases of an MB-1 rocket from a 0.04956-scaled model of the Convair F-106A airplane at Mach number 1.59 : COORD. No. AF-AM-57
- Exploratory investigation of static- and base-pressure increases resulting from combustion of aluminum borohydride adjacent to body of revolution in supersonic wing tunnel
- Flight-determined static lateral stability and control characteristics of a swept-wing fighter airplane to a Mach number of 1.39
- Flight data pertinent to buffeting and maximum normal-force coefficient of the Douglas X-3 research airplane
- Flight-determined induction-system and surge characteristics of the YF-102 airplane with a two-spool turbojet engine
- Comparison of low-lift drag at Mach numbers from 0.74 to 1.37 of rocket-boosted models having externally braced wings and cantilever wings
- Flight evaluation of the lateral stability and control characteristics of the Convair YF-102 airplane
- A flight study of longitudinal-control-system dynamic characteristics by the use of a variable-control-system airplane
- Flow-turning losses associated with zero-drag external-compression supersonic inlets
- Free-jet tests of a 1.1-inch-diameter supersonic ram-jet engine
- Theoretical analysis of one-stage windmills for reducing flow distortion