Frederick O. Smetana

Analysis of flight vehicle performance and aerodynamic control

Flight vehicle performance and aerodynamic control

Reston, Va: American Institute of Aeronautics and Astronautics.

Introductory aerodynamics and hydrodynamics of wings and bodies: A software-based approach

Reston, Va.: American Institute of Aeronautics and Astronautics.

Introduction to the control of dynamic systems

Using the computer to enhance the learning of engineering concepts: Some examples

Computer Applications in Engineering Education, 1(4), 321–329.

Aircraft performance, stability and control

Aircraft performance, stability, and contro

Monterey, Calif: Aircraft Designs, Inc.

An improved panel method for determining the drag of isolated bodies at small angles of attack

International Symposium on Computational Fluid Dynamics : Sep. 9-12, 1985, Kenchiku-Kaikan, Tokyo. Tokyo : Japan Society of Computational Fluid Dynamics.

Computer-assisted analysis of aircraft performance, stability, and control

Automated design of minimum drag light aircraft fuselages and nacelles

NASA Contractor Report, CR1 68913(May).

Design of minimum drag fairings for specific payload packages

Conference proceedings : IEEE Southeastcon '82, April 4-7, 1982, Sandestin, Destin, Florida., 134–139. New York : ?b Institute of Electrical and Electronics Engineers.

Fortran codes for classical methods in linear dynamics

Analytical studies on the effects of cooling flows on light aircraft drag

SAE Business Aircraft Conference, (April).

Integration of propeller slipstreams into the aerodynamic analysis of bodies

SAE Business Aircraft Conference, (April).

A Study of optimum cowl shapes and flow port locations for minimum drag and effective engine cooling., Volume I.

NASA Contractor Report, CR 159379(November).

A home-size solar-powered engine for cooling systems or generation of electricity

Mechanics of bimodulus materials : ?b presented at the ASME winter annual meeting, New York, New York, December 2-7, 1979. New York: ASME.

An analytical investigation of the the effectiveness of solar collectors as nighttime heat radiators

NASA Contractor Report, CR 3111(March).

Flight evaluation of predicted light aircraft drag, performance, and stability

NASA Contractor Report, CR 158076(May).

Recent results obtained with a new method for measuring power and drag in flight

SAE Business Aircraft Conference, (April).

Results of heating mode performance tests of a solar-assisted heat pump

NASA Contractor Report, CR 3112(April).

An economic and performance study of solar preheaters for domestic hot water heaters in North Carolina

NASA Contractor Report, CR 2813(March).

Comparison of a new method for measuring aircraft power in flight with a standard technique

SAE Business Aircraft Conference, (March).

Comparison of predicted with measured aerodynamic characteristics of the ATLIT airplane

SAE Business Aircraft Conference, (March).

Prediction of light aircraft tail onset flows ? a review and analysis

NASA Contractor Report, CR 2774(April).

Take advantage of low-cost information

Industrial Engineering, 9(11), 36–38.

A new wind energy system, department of mechanical and aerospace engineering report

NASA Contractor Report, CR 146539(November).

Drag analysis methods for light aircraft

SAE Business Aircraft Conference, (April).

Light aircraft lift, drag, and moment prediction ? a review and analysis

NASA Contractor Report, CR 2523(May).

Mapping individual logical processes

Educational and Psychological Measurement, 35(August), 679–682.

Nacelle drag reduction: An analytically-guided experimental program

Proceedings of the NASA?Industry?University General Aviation Drag Reduction Workshop : July 14-16, 1975, Space Technology Center, University of Kansas, 257–261. Lawrence : Space Technology Center, University of Kansas.

Prospects and time tables for analytical estimation of the drag of complete aircraft configurations

Proceedings of the NASA?Industry?University General Aviation Drag Reduction Workshop : ?b July 14-16, 1975, Space Technology Center, University of Kansas, 39–41. Lawrence : Space Technology Center, University of Kansas.

Solar assisted heat pumps: A possible wave of the future, department of mechanical and aerospace engineering report

NASA Contractor Report, CR 2771(December).

Storage of summertime waste heat from electric generating plants for use in wintertime

AIAA 10th Thermophysics Conference [held in] Denver, Colorado, May 27-29, 1975. New York, American Institute of Aeronautics and Astronautics.

Turbo jet engine gas path analysis ? a review and analysis

AGARD conference proceedings, 165, 16–11-1613.

A study of the relative effectiveness and costs of computerized information retrieval in the interactive mode North Carolina Science and Technology Research Center Report STR-505

NASA Contractor Report, CR 142206(November).

Industrial noise control: Some case histories. Vol. 1, North Carolina Science and Technology Center Report STR-504

NASA Contractor Report, CR 142314(August).

Mapping individual logical processes in information searching North Carolina Science and Technology Research Center Report STR-506

NASA Contractor Report, CR 142207(November).

A designstudy for a simply-to-fly, constant-attitude aircraft

NASA Contractor Report, CR 2208(March).

An analytical study of the response of a constant-attitude aircraft to atmospheric turbulence

NASA Contractor Report, CR 2204(March).

Equilibrium concentrations of N2H4 and its decomposition products at elevated pressures and temperatures, Department of Mechanical and Aerospace Engineering Report

NASA Contractor Report, CR 135478(May).

Point and path performance of light aircraft ? a review and analysis

NASA Contractor Report, CR 2272(June).

Toward simpler techniques for the prediction of lift, drag, and moment characteristics of airfoils at transonic speeds

Journal of Aircraft, 10(2), 124–126.

A fast-acting electrical servo for the actuation of full-span fowler type wing flaps in DLC applications ? a detail design study

NASA Contractor Report, CR 2059(July).

Automated prediction of light aircraft performance and riding and handling qualities

SAE Business Aircraft Conference, (April).

Characteristics of an arc-heatedfreejetissuing from a supersonic nozzle

Air Force Office of Scientific Research (AFOSR), TR-72(July).

Development of computer programs to determine the aerodynamic characteristics of complete light aircraft: Final report

NASA Contractor Report, CR 139690(August).

Flight testing for the evaluation of light aircraft stability derivatives ? a review and analysis

NASA Contractor Report, CR 2016(May).

Riding and handling qualities of light aircraft

NASA Contractor Report, CR 1975(March).

The performance of a nude ionization gauge in a low temperatureenvironment, proceedings of the eighth international symposium on rarefied gas dynamics

Air Force Office of Scientific Research (AFOSR), TR-72(July).

A correlation of recent results on the mass flow and pressure distribution in the transition regime

Rarefied gas dynamics : proceedings of the seventh International Symposium on Rarefied Gas Dynamics held at the University of Pisa, June 19-July 3, 1970, 241–249. Pisa, Italy : Editrice tecnico scientifica.

A flight control system providing a simple-to-fly constant attitude aircraft

SAE Business Aircraft Conference, (March).

Observations on the effects of pressure ratio and upstream flow conditions on the acoustical response of closed pipes

Journal of the Acoustical Society of America, (February), 399–401.

The entrainment and trapping of helium by a condensing gas stream

Rarefied gas dynamics : proceedings of the seventh International Symposium on Rarefied Gas Dynamics held at the University of Pisa, June 19-July 3, 1970, 1023–1031. Pisa, Italy : Editrice tecnico scientifica.

A study of NACA and NASA published information of pertinence in the design of light aircraft, Vol. 1: Structures

NASA Contractor Report, CR-1484(March).

Experiments on the current collected by a cylindrical languir probe in a rarefied plasma streaming with high velocity

Advances in Applied Mechanics. Supplements, 5, 1783–1790.

Literature search for theses by computer?results of the first two years of the program

Proceedings of the American Society for Information Science, 6, 95–100.

Results of a numerical experiment to determine the current collected in a charged cylinder in a collisionless plasma stream

Advances in Applied Mechanics. Supplements, 5, 1627–1636.

State-of-the-art review of turbine engine checkout techniques

AIAA Paper, 69-581.

Temperature effects on ionization gauge performance at low pressures

Journal of Vacuum Science & Technology, 6(5), 874–878.

Effects of downstream geometry on rarefied gas flow through a nozzle throat

AIAA Journal, 6(7).

Pressure sensitivity in ionization gauges

Journal of Vacuum Science & Technology, 5(2), 62–64.

Results of an experiment to provide low cost computer searches of the NASA information file to university graduate students in the Southeast

NASA Contractor Report, CR-95724(July).

Measurements of the discharge characteristics of sharp-edged and round-edged orifices in the transition regime, rarefied gas dynamics

Advances in Applied Mechanics. Supplements, 4, 1243–1254.

Turbine engine checkout

Ft. Belvoir Defense Technical Information Center.

An absolute high resolution calibrator for vacuum gauges

Journal of Vacuum Science & Technology, 3(2), 49–53.

On the determination of parachute cloth permeability

Zeitschrift Fu?r Flugwissenschaften, 14(10), 429–435.

Transition regime flow through a short tube with a bell mouth entry

AIAA Journal, 4(1).

low-rate gas flow meter

Journal of Vacuum Science & Technology, 3(6), 357–359.

Results of a research program to develop the aerodynamic configuration of a pitot-static tube capable of accurate operation to mach number 5 and 150,000 ft.

Journal of the Royal Aeronautical Society, (March), 200–201.

Theoretical study of a convergentnozzle and free jet flow

Proceedings of the fluid amplification symposium, 5–28. Washington : Army Materiel Command, Harry Diamond Laboratories.

A study of means for measuring electron density in a 24? diameter arc-heated hypersonic wind tunnel

Proceedings of the 1st International Congress on Instrumentation in Aerospace Simulation Facilities, Paris, 28-29 Sept. 1964, E?cole Nationale Superie?ure de l'Ae?ronautique. Alexandria, Va. : Defense Documentation Center, Defense Supply Agency.

Aerodynamic characteristics of representative parachute fabrics at simulated altitudes

Proceedings of the Fifth International Symposium on Space Technology and Science : Tokyo, 1963. Tokyo, Japan : Distributed by AGNE Corp.

An approach to the measurement of air data parameters for guidance and navigation during atmospheric reentry

Proceedings of the Fifth International Symposium on Space Technology and Science : Tokyo, 1963., 259–272. Tokyo, Japan : Distributed by AGNE Corp.

Comments on flow nozzles with zero beta ratio

Journal of Basic Engineering, (September).

Comments on angle of attack and sideslip from pressure measurements on a fixed hemispherical nose

AIAA Journal, 1(3).

Convergent-divergent nozzle dischargecharacteristics in the transition regime between free molecule and contiuum flow

Use of models and scaling in shock and vibration. ?b Papers presented at a colloquium on use of models and scaling in shock and vibration at the Winter annual meeting of the ASME, Philadelphia, Pennsylvania, Tuesday, November 19, 1963. New York: ASME.

EGF flow analysis program

ASD Technical Report, 63-794,(August).

On the current collected by a charged cylinder immersed in a two-dimensional rarefied plasmastream

Advances in Applied Mechanics. Supplements, 2, 65–90.

On the prediction of gas flow rates through round wire screens

Journal of Basic Engineering, (December), 620–624.

A calibration facility for high resolution vacuum gauges

USCEC Report, 83-214(July).

A preliminary investigation of the effects of variations in Reynolds numbers and surface temperature on four surface pressures on a slightly blunted 7 1/2 degree half-angle cone at mach numbers 5 and 8 and angles of attack up to 24 degrees

ASD Technical Report, TR 62-360(May).

Comment on comparison of flow direction probes at supersonic speeds

Journal of the Aerospace Sciences, 29(5), 625–626.

Pressure lag through orifices and short tubes for small pressure ratios and flow conditions from free molecule to continuum

USCEC Report, 83-211(January).

A semi-empirical description of the discharge characteristics of a low-density hypersonic nozzle

Journal of the Aerospace Sciences, (December), 988–989.

Experimental study of heating a gas flow by high frequency discharge

AEDC TR, 61-11(September).

Theoretical and experimental study of gas flow through cloth over a Range of Pressure and Temperatures

ASD Technical Report, TR 61-192(June).

Properties of the plasma sheath and its effects on the transmission of electromagnetic waves

USCEC Report, 85-101(April).

Studies in the heating of a supersonic gas stream by a radio frequency discharge

Air Force Office of Scientific Research (AFOSR), TN 60-648(June).

Design and test of aerodynamically-compensated pitot-static tubes for four service aircraft

WADC Technical Report, (May).

Experiments on a radio frequency discharge plasma in supersonic flow

1959 Heat Transfer and Fluid Mechanics Institute : ?b preprints of papers. Stanford, Calif. : Stanford University Press for the Heat Transfer and Fluid Mechanics Institute.

Some further results on heating a supersonic gas stream with a radio frequency discharge

Air Force Office of Scientific Research (AFOSR), TN 59-1127(November).

A further study of angle-ofattack, angle-of-sideslip, pitot-static probes

WADC Technical Report, (June).

A furtherstudy ofangle-of-attack, angle-of-sideslip, pitot-static probes. Supplement I: Calibration of the USCEC head at transonic speeds

WADC Technical Report, (June).

Design of aerodynamic static pressure compensation for service aircraft

Proceedings of I.S.A. fourth national flight test instrumentation symposium. Pittsburgh : I.S.A.

Final report: Investigation of circulation control

USCEC Report, 49-101.

Investigation of free-stream and stagnation pressure measurement from transonic and supersonic aircraft. Final report

WADC Technical Report, (April).

A Study of angle-of-attack and angle-of-sideslip pitot-static probes

WADC Technical Report, (January).

Investigation of free stream and stagnation pressure measurement from transonic and supersonic aircraft. Phase III: Development and flight test of aerodynamic static pressure compensation for a service type aircraft

WADC Technical Report, (September).

Investigation of circulation control

USCEC Report, 49-8(June).

Determination of frequency response characteristics, including coupling tendencies, during standard Air Force phase tests, with results on F-86D at M =0.85

Air Force Technical Note AFFTC, TR 54-19(May).

Investigation of supersonic diffuserinstability

USCEC Report, 41-5(August).

Longitudinal and directional frequency response characteristics of an F-86D

Air Force Technical Note AFFTC, N 55-29(December).

experimental longitudinal frequency response characteristics of the F-94C aircraft

Air Force Technical Note AFFTC, 55-1(February).

An explanation of the theory and applications of dynamic response flight testing

Air Force Technical Note AFFTC, 54-1(May).

Determination of neutral points and maneuver points from longitudinally accelerated flight data

Air Force Technical Note AFFTC, R-19(July).

C-12 a final structural inegrity demonstration flight tests

Douglas Aircraft Company Report, Dev 960(February).

A Study of theses produced at three universities for possible commercial applications

Smetana, F. O. NASA Contractor Report, CR 95703.

A study of fluidic whistles as temperature sensors

Daggerhart, J. A., & Smetana, F. O. NASA Contractor Report, CR 112383.

An experimental study of the cryoentrainment pump

Daggerhart, J. A., & Smetana, F. O. NASA Contractor Report, CR 66873.

Literature search performance as affected by searcher?s background

Smetana, F. O. NASA Contractor Report, CR 155960.

Literature searches for theses by computer: Second year of the program

Smetana, F. O., & Walker, S. R. NASA Contractor Report, CR 106262.