Free-flight Investigation of the Longitudinal Stability and Control of a Rocket-propelled Missile Model Having Cruciform, Triangular, Interdigitated Wings and Tails
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Sandahl, Carl A↗
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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Free-flight-tunnel investigation of the dynamic lateral stability and control characteristics of a tip-to-tip bomber-fighter coupled airplane configuration
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Bennett, Charles V↗
Free-flight Measurements at Mach Numbers from 0.7 to 1.6 of Some Effects of Airfoil-thickness Distribution and Trailing-edge Angle on Aileron Rolling Effectiveness and Drag for Wings with 0 and 45 Degrees Sweepback
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Fields, E M↗
Base Pressures Measured on Several Parabolic-arc Bodies of Revolution in Free Flight at Mach Numbers from 0.8 to 1.4 and at Large Reynolds Numbers
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Katz, Ellis↗
Instrumentation of the Ames Supersonic Free-flight Wind Tunnel
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Briggs, Robert O↗
Free-flight Investigation to Determine Force and Hinge-moment Characteristics at Zero Angle of Attack of a 60 Degrees Sweptback Half-delta Tip Control on a 60 Degrees Sweptback Delta Wing at Mach Numbers Between 0.68 and 1.44
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Martz, C William↗
Free-flight Investigation of Longitudinal Stability and Control of a Rocket-propelled Missile Model Having Cruciform, Triangular, Inline Wings and Tails
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Hall, James R↗
The Ames Supersonic Free-flight Wind Tunnel
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Seiff, Alvin↗
Free-flight Investigation of the Zero-lift Drag of Several Wings at Supersonic Mach Numbers Extending to 2.6
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Hopko, Russell N↗
Use of an Aerodynamically Pulsed All-movable Horizontal Tail to Obtain Longitudinal Characteristics of Rocket-powered Models in Free Flight and Some Initial Results from an Arrow-wing-body-tail Configuration
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Gillespie, Warren, Jr↗
Effects of Stabilizing Fins and a Rear-support Sting on the Base Pressure of a Body of Revolution in Free Flight at Mach Numbers from 0.7 to 1.3
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Hart, Roger G↗
Free-flight-tunnel investigation of the dynamic lateral stability and control characteristics of a high-aspect-ratio bomber model with a sweptback-wing fighter model attached to each wing tip
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Bennett, Charles V↗
Longitudinal stability and control characteristics of a canard missile configuration for Mach numbers from 1.1 to 1.93 as determined from free-flight and wind-tunnel investigation
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Curfman, Howard J , Jr↗
Free-flight measurements of some effects of spoiler span and projection and wing flexibility on rolling effectiveness and drag of plain spoilers on a tapered sweptback wing at Mach numbers between 0.6 and 1.6
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Schult, Eugene D↗
The Longitudinal Stability and Control Characteristics of a 60 Degree Delta-wing Missile Having Half-delta Tip Controls as Obtained from a Free-flight Investigation at Transonic and Supersonic Speeds
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Moul, Martin T↗
A Free-flight Investigation at Zero Lift in the Mach Number Range Between 0.7 and 1.4 to Determine the Effectiveness of an Inset Tab as a Means of Aerodynamically Relieving Aileron Hinge Moments
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Bland, William M , Jr↗
Initial Flutter Tests in the Langley Transonic Blowdown Tunnel and Comparison with Free-flight Flutter Results
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Bursnall, William J↗
Effects of Wing Elasticity on the Aerodynamic Characteristics of an Airplane Configuration Having 45 Degrees Sweptback Wings as Obtained from Free-flight Rocket-model Tests at Transonic Speeds
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Vitale, A James↗