Theoretical prediction of interference loading on aircraft stores: Part I - Subsonic speeds

Computer program is developed for theoretically predicting loading on pylon-mounted stores in subsonic compressible flow. Linear theory predicts flow field produced by aircraft wing, nose, inlet, and pylons. Program was written in FORTRAN IV for CDC 6000 computer

Theoretical prediction of interference loading on aircraft stores: Part II - Supersonic speeds

Linear theory is used, without two dimensional or slender body assumptions, to predict flow field produced by aircraft wing, nose, inlet, and pylons. Aircraft shock wave locations are predicted, and their effect on flow field is included through transformation of aircraft geometry. Program was written in FORTRAN IV for CDC 6400 computer

The Influence of Socioeconomic Factors on Fear of Falling and Mobility Outcomes after Lower Limb Loss: a Preliminary Study

Background and Purpose: Current research has revealed that as much as 52.4% of individuals with lower limb loss report falling at least once in the past year. Previous research has also indicated that rehabilitation, including physical therapy (PT), generally improves patient outcomes after definitive amputation. Socioeconomic status has been shown to be an important factor in accessing healthcare but has yet to be investigated in this population. The purpose of this study was to investigate the effects of socioeconomic status and access to PT, and how limb loss affects mobility and fear of falling perception. We hypothesized: [1] individuals with socioeconomic difficulty would have reduced access to PT after amputation, and [2] individuals with limb loss will have increased fear of falling and decreased mobility performance when compared to non-amputee, age-matched controls. Subjects: 23 participants (7 females,16 males) mean age 51.30 years old (+ 13.17 SD, range 22-70) with lower limb loss ambulating with a definitive prosthesis. Materials/Methods: Participants completed a survey that included the Fear of Falling Avoidance Behavior Questionnaire (FFABQ), questions to determine their socioeconomic status, and whether they received PT after amputation. Mobility outcomes were measured using the standardized Timed Up and Go test (TUG) and the Six Minute Walk Test (6MWT). Results: There was no statistically significant difference in access to PT after amputation between those with and without financial difficulty (p=.354). However, 75% of participants who had no socioeconomic difficulty reported receiving PT, in comparison to only 25% in those who had socioeconomic difficulty. Additionally, 34.8% of our participants reported socioeconomic difficulties. When comparing the participants with amputation to the non-amputee, age-matched controls, there was a significant difference in the TUG (p\u3c.001), 6MWT (p\u3c.001), and FFABQ (p=.008). On average, participants with limb loss were 4.4 seconds slower on the TUG, walked 136.4m less on the 6MWT, and had an increased FFABQ score of 6.6 points out of 56 points. Discussion: Access to physical therapy and socioeconomic status have been overlooked in current literature for individuals after amputation. While the effect of socioeconomic status on PT access did not reach statistical significance in this preliminary study, only 25% of those who reported socioeconomic difficulty received physical therapy after amputation, compared to 75% in those who reported no difficulty. Further research is needed to determine whether low socioeconomic status is predictive of receiving rehabilitation services post-amputation and long-term outcomes. Our findings also showed that when compared to age-matched non-amputees, amputees tend to have impaired mobility and higher degree of fear of falling. These findings agree with current literature. Conclusion: Although not statistically significant, our preliminary findings showed that socioeconomic difficulty may affect access to physical therapy after amputation. Furthermore, our data demonstrated that individuals with lower limb loss exhibit reduced mobility performance and increased fear of falling when compared to the age-matched controls

Subsonic aerodynamic characteristics of a proposed advanced manned launch system orbiter configuration

The Advanced Manned Launch System is a proposed near-term technology, two-stage, fully reusable launch system that consists of an unmanned glide-back booster and a manned orbiter. An orbiter model that featured a large fuselage and an aft delta wing with tip fins was tested in the Langley 7- by 10-Foot High-Speed Tunnel. A crew cabin, large payload fairing, and crew access tunnel were mounted on the upper body. The results of the investigation indicated that the configuration was longitudinally stable to an angle of attack of about 6 deg about a center-of-gravity position of 0.7 body length. The model had an untrimmed lift-drag ratio of 6.6, but could not be trimmed at positive lift. The orbiter model was also directionally unstable. The payload fairing was responsible for about half the instability. The tip-fin controllers, which are designed as active controls to produce artificial directional stability, were effective in producing yawing moment, but sizable adverse rolling moment occurred at angles of attack above 6 deg. Differential deflection of the elevon surfaces was effective in producing rolling moment with only small values of adverse yawing moment

Subsonic longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration having spanwise leading-edge vortex enhancement

A configuration which integrates a close coupled canard wing combination, spanwise blowing for enhancement of the wing leading edge vortex, an engine-over-wing concept, and a wing trailing edge coanda-effect flap is studied. The data on the configuration are presented in tabular from without discussion. The investigation was conducted in the Langley 7- by 10-foot high speed tunnel at a Mach number of 0.166 through an angle-of-attack range from -2 to 22 deg. Rectangular main engine nozzles of aspect ratio 4, 6, and 8 were tested over a momentum coefficient range from 1.0 to 1.8

A Green's function formulation for a nonlinear potential flow solution applicable to transonic flow

Routine determination of inviscid subsonic flow fields about wing-body-tail configurations employing a Green's function approach for numerical solution of the perturbation velocity potential equation is successfully extended into the high subsonic subcritical flow regime and into the shock-free supersonic flow regime. A modified Green's function formulation, valid throughout a range of Mach numbers including transonic, that takes an explicit accounting of the intrinsic nonlinearity in the parent governing partial differential equations is developed. Some considerations pertinent to flow field predictions in the transonic flow regime are discussed

Subsonic maneuver capability of a supersonic cruise fighter wing concept

A theoretical and experimental investigation was conducted of the subsonic maneuver capability of a fighter wing concept designed for supersonic cruise. To improve the subsonic maneuver capability, the wing utilized full-span leading- and trailing-edge flaps that were designed with the aid of a subsonic-analysis computer program. Wind-tunnel tests were made at Mach numbers of 0.3, 0.5, and 0.7. Force and moment data obtained were compared with theoretical predictions of Mach 0.5 from two subsonic-analysis computer programs. The two theoretical programs gave a good prediction of the lift and drag characteristics but only a fair prediction of the pitching moment. The experimental results of this study show that with the proper combination of leading- and trailing-edge flap deflections, a suction parameter of nearly 90 percent can be attained at a Mach number of 0.5 and a lift coefficient of 0.73; this is a three-fold improvement from 30 percent for the basic wing

Oktibbeha County Area Brochure

Starkville, Mississippi State College, County of Oktibbeha.https://scholarsjunction.msstate.edu/ua-vertical-file/1067/thumbnail.jp

The Little Shepherd of Kingdom Come

This powerful novel is one of the most perceptive tellings of the Civil War experience. John Fox Jr. (1863–1919), author of The Trail of the Lonesome Pine and many other books, remains one of Kentucky best-known and most popular writers. The war and its conflicts set an epic stage for the novel\u27s main business, the testing and maturation of a hero. -- Kentucky Living Makes one realize as never before the agonizing effects of the Civil War in a border state. -- New York Timeshttps://uknowledge.uky.edu/upk_american_literature/1018/thumbnail.jp

The Heart of the Hills

First published in 1913, The Heart of the Hills is the last novel completed by John Fox Jr. and the final piece in his mountain trilogy. This companion to The Little Shepherd of Kingdom Come and The Trail of the Lonesome Pine is crucial to an understanding of Fox\u27s views. In The Heart of the Hills Fox revises his earlier thoughts about mountain people. He depicts more clearly than in his previous work just how they were exploited by outside industrialists-those men who, in the words of Fox\u27s hero Jason Hawn, got rich diggin\u27 our coal an\u27 cuttin\u27 our timber. He also reveals the long-term impact of this exploitation on the environment. Having witnessed the ravages of clearcutting on his travels through the mountain country of Kentucky and Virginia in 1911-1912, Fox was all the more receptive to the warnings voiced by his environmentally conscious father. From their letters and diaries it is clear that John Fox Sr.\u27s influence permeates The Heart of the Hills; in this work, dedicated to his dying father, Fox determined to make amends to the mountain people. John Fox Jr. (1863–1919), author of The Little Shepherd of Kingdom Come, The Trail of the Lonesome Pine, and many other books, remains one of Kentucky best-known and most popular writers. Welcome for readers interested in Kentucky authors and Appalachian literature. A very fine foreword by Darlene Wilson adds much to our understanding of Fox\u27s impetus for writing this particular book at this particular time. —Register of the Kentucky Historical Societyhttps://uknowledge.uky.edu/upk_english_language_and_literature_north_america/1047/thumbnail.jp