Reingestion characteristics and inlet flow distortion of V/STOL lift-engine fighter configurations
Reingestion characteristics and inlet flow distortion of V/STOL fighter powered by J-85 engine
Barrack, J. P.↗
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Approximate treatment of V/STOL wall interference for closed circular tunnels
Characteristics of V/STOL wall interference for closed circular wind tunnels
Heyson, H. H.↗
Flight investigation of a V/STOL transport model with four pod-mounted lift fans
Flight characteristics of V/STOL transport model with four pod-mounted lift fans
Grafton, S. B.↗
Computer program for preliminary design and analysis of V/STOL tip-turbine fans
Computer program for design and analysis of V/STOL tip turbine fans
Auer, B. M.↗
Aerodynamic characteristics of a large-scale V/STOL transport model with tandem lift fans mounted at mid-semispan of the wing
Aerodynamic characteristics of V/STOL transport model with tandem lift fans mounted at mid-semispan of wing
Dickinson, S. O.↗
An algorithm for digital resolution of range for V/STOL aircraft
Algorithm for digital resolution of range for V/STOL aircraft
Bondi, M. J.↗
Practical engineering methods for predicting hot gas reingestion characteristics of V/STOL aircraft jet lift engines
Engineering methods for predicting temperatures and velocities in vicinity of vertical lift engines of jet V/STOL aircraft operating near ground
Gray, L.↗
Vibration in V/STOL aircraft
Environmental tests of V/STOL vibration effects on human comfort
Jones, W. L.↗
An airspace utilization model for V/STOL terminal operations
Computer graphics display program for use in terminal operations and V/STOL approach and departure path synthesis
De Maio, D. A.↗
Stability and control characteristics of STOL and V/STOL airplanes
Stability, control, and handling quality characteristics of STOL and V/STOL airplanes
Chambers, J. R.↗
Lewis 9- by 15-foot V/STOL wind tunnel
Lewis 9 by 15 foot V/STOL wind tunnel in return leg of supersonic wind tunnel
Clough, N.↗
Aerodynamics of lift fan V/STOL aircraft
Aerodynamic characteristics of lift fan installation for direct lift V/STOL aircraft
Kirk, J. V.↗
Operations of V/STOL aircraft in the terminal area
Terminal area operations of V/STOL aircraft, considering approaches, approach speeds, wind and velocity effects and noise
Garren, J. F. JR.↗
Control of V/STOL aircraft in turbulence
V/STOL aircraft flight path and attitude controls in turbulence, discussing design based on state variable methods of control theory
Swaim, R. L.↗
Aerodynamics of lift fan V/STOL aircraft
V/stol aircraft lift fan aerodynamics, discussing optimum fan pressure ratios, augmentation ratio, noise constraints, wing loading and fan configurations
Hall, L. P.↗
Operational procedure for computer program for design point characteristics of a compressed-air generator with through-flow combustor for V/STOL applications
The computer program described in this report calculates the design-point characteristics of a compressed-air generator for use in V/STOL applications such as systems with a tip-turbine-driven lift fan. The program computes the dimensions and mass, as well as the thermodynamic performance of a model air generator configuration which involves a straight through-flow combustor. Physical and thermodynamic characteristics of the air generator components are also given. The program was written in FORTRAN IV language. Provision has been made so that the program will accept input values in either SI units or U.S. customary units. Each air generator design-point calculation requires about 1.5 seconds of 7094 computer time for execution.
Krebs, R. P.↗
Fundamental limitations on V/STOL terminal guidance due to aircraft characteristics
A review is given of limitations on approach flight paths of V/STOL aircraft, including limits on descent angle due to maximum drag/lift ratio. A method of calculating maximum drag/lift ratio of tilt-wing and deflected slipstream aircraft is presented. Derivatives and transfer functions for the CL-84 tilt-wing and X-22A tilt-duct aircraft are presented. For the unaugmented CL-84 in steep descents the transfer function relating descent angle to thrust contains a right-half plane zero. Using optimal control theory, it is shown that this zero causes a serious degradation in the accuracy with which steep flight paths can be followed in the presence of gusts.
Wolkovitch, J.↗