#
Stability of airplanes, Longitudinal
Resource Information
The concept ** Stability of airplanes, Longitudinal** represents the subject, aboutness, idea or notion of resources found in **University of Oklahoma Libraries**.

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Stability of airplanes, Longitudinal
Resource Information

The concept

**Stability of airplanes, Longitudinal**represents the subject, aboutness, idea or notion of resources found in**University of Oklahoma Libraries**.- Label
- Stability of airplanes, Longitudinal

- Authority link
- http://id.worldcat.org/fast/01131217

- Source
- fast

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- Wind-tunnel investigation of the static longitudinal and lateral stability of a 1/62-scale model of the X-1E at supersonic speeds
- A transonic wind-tunnel investigation of the longitudinal force and moment characteristics of two delta wings and one clipped-tip delta wing of 4 percent thickness on a slender body
- Aerodynamic characteristics at small scale and a Mach number of 1.38 of untapered wings having M and W plan forms
- An investigation at Mach numbers 1.94 and 2.41 of jet effects upon the longitudinal and directional stability of a general aircraft configuration employing wing-tip-mounted nacelles
- Analog-computer investigation of effects of friction and preload on the dynamic longitudinal characteristics of a pilot-airplane combination
- Charts and approximate formulas for the estimation of aeroelastic effects on the loading of swept and unswept wings
- Compressibility effects on the longitudinal stability and control of a pursuit-type airplane as measured in flight
- Damping-in-pitch characteristics at high subsonic and transonic speeds of four 35° sweptback wings
- Effect of horizontal-tail location on low-speed static longitudinal stability and damping in pitch of a model having 45° sweptback wing and tail surfaces
- Effect of horizontal-tail size and tail length on low-speed static longitudinal stability and damping in pitch of a model having 45° sweptback wing and tail surfaces
- Effects of fences, leading-edge chord-extensions, bound-layer ramps, and trailing-edge flaps on the longitudinal stability of a twisted and cambered 60° sweptback-wing--indented-body configuration at transonic speeds
- Effects of twist and camber on the low-speed longitudinal stability characteristics of a 45° swept-back wing of aspect ratio 8 at Reynolds numbers from 1.5 x 106 to 4.8 x 10 as determined by pressure distributions, force tests, and calculations
- Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration
- Effects of wing-tip droop on the longitudinal characteristics of two highly swept wing-body combinations at Mach numbers from 0.6 to 1.4
- Lift, drag, and static longitudinal stability data from an exploratory investigation at a Mach number of 6.86 of an airplane configuration having a wing of trapezoidal plan form
- Longitudinal aerodynamic characteristics of a model airplane configuration equipped with a scaled X-1 airplane wing
- Longitudinal stability and control characteristics from a flight investigation of a cruciform canard missile configuration having an exposed wing-canard area ratio of 16:1
- Longitudinal stability and trim of two rocket-propelled airplane models having 45° sweptback wings and tails with the horizontal tail mounted in two positions
- Longitudinal stability characteristics at transonic speeds of a rocket-propelled model of an airplane having a 45 degree swept wing of aspect ratio 6.0
- Low-speed pitching derivatives of low-aspect-ratio wings of triangular and modified triangular plan forms
- Matrix method of determining the longitudinal-stability coefficients and frequency response of an aircraft from transient flight data
- Measurement of the longitudinal moment of inertia of a flexible airplane
- Notes on longitudinal stability and balance
- Power-on longitudinal-stability and control tests of the 1/8-scale model of the Brewster F2A airplane equipped with full-span slotted flaps and a new horizontal tail
- Preliminary results for a free-flight investigation at transonic and supersonic speeds of longitudinal stability and control characteristics of an airplane configuration with a thin straight wing of aspect ratio 3
- Rocket-model investigation of longitudinal stability and drag characteristics of an airplane configuration have a 60° delta wing and a high unwept horizontal tail
- Some effects of aircraft configuration on static longitudinal and directional stability characteristics at supersonic Mach numbers below 3
- Some effects of fin plan form on the static stability of fin-body combinations at Mach number 4.06
- Some effects of tail height and wing plan form on the static longitudinal stability characteristics of a small-scale model at high subsonic speeds
- Some low-speed wind-tunnel experiments pertaining to the longitudinal stability characteristics of a 35° swept-wing model and an unswept-wing model
- Static investigation of several jet deflectors for longitudinal control of an aircraft
- The effect of longitudinal moment of inertia upon dynamic stability
- The effect of nose radius and shape of the aerodynamic characteristics of a fuselage and a wing-fuselage combination at angles of attack
- The effects of fuselage size on the low-speed longitudinal aerodynamic characteristics of a thin 60° delta wing with and without a double slotted flap
- The static and dynamic longitudinal stability characteristics of some supersonic aircraft configurations
- Three-degree-of-freedom evaluation of the longitudinal transfer functions of a supersonic canard missile configuration including changes in forward speed
- Total energy-rate feedback for automatic glide-slope tracking during wind-shear penetration
- Transonic longitudinal aerodynamic characteristics of a fighter-type airplane model with a low-aspect-ratio unswept wing and tee-tail
- Transonic longitudinal aerodynamic effects of sweeping up the rear of the fuselage of a rocket-propelled airplane model having no horizontal tail
- Transonic wind-tunnel investigation of an unswept wing in combination with a systematic series of four bodies
- Transonic wind-tunnel investigation of the interference between a 45° sweptback wing and a systematic series of four bodies

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