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title: nasa research memorandum

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Bibliography of NACA papers on rotating-wing aircraft, January 1952

Gessow, Alfred | TIBKAT | 1952

Schlagwörter: NACA-Profil

Systematic two-dimensional cascade tests of NACA 65-series compressor blades at low speeds

Herrig, L. Joseph / Emery, James C. / Erwin, John R. | TIBKAT | 1951

Schlagwörter: NACA-Profil

An NACA transonic test section with tapered slots tested at Mach numbers to 1.26

Ward, Vernon G. / Whitcomb, Charles F. / Pearson, Merwin D. | TIBKAT | 1950

Schlagwörter: NACA-Profil

Impingement of water droplets on an NACA 65 1-212 airfoil at an angle of attack of 4°

Brun, Rinaldo J. / Serafini, John S. / Moshos, George J. | TIBKAT | 1952

Schlagwörter: NACA-Profil

Effect of section thickness and trailing-edge radius on the performance of NACA 65-series compressor blades in cascade at low speeds

Herring, L. Joseph / Emery, James C. / Erwin, John R. | TIBKAT | 1951

Schlagwörter: NACA-Profil

Flight measurements of average skin-friction coefficients on a parabolic body of revolution (NACA RM-10) at Mach numbers from 1.0 to 3.7

Loposer, J. Dan / Rumsey, Charles B. | TIBKAT | 1954

Schlagwörter: NACA-Profil

NACA 65-series compressor rotor performance with varying annulus-area ratio, solidity, blade angle, and Reynolds number and comparison with cascade results

Schulze, Wallace M. / Erwin, John R. / Ashby, George C. | TIBKAT | 1953

Schlagwörter: NACA-Profil

An investigation of several NACA 1-series inlets at Mach numbers from 0.4 to 1.29 for mass-flow ratios near 1.0

Re, Richard J. | TIBKAT | 1975

Schlagwörter: NACA-Profil

Fuselage pressures measured on the Bell X-1 research airplane in transonic flight

Knapp, Ronald J. / Jordan, Gareth H. / Johnson, Wallace E. | TIBKAT | 1953

Flight measurements of pressures on base and rear part of fuselage of the Bell X-1 research airplane at transonic speeds, including power effects

Knapp, Ronald J. / Johnson, Wallace E. | TIBKAT | 1953

A transonic wind-tunnel investigation of the longitudinal stability and control characteristics of a 0.09-scale model of the Bell X-5 research airplane and comparison with flight

Bielat, Ralph P. / Campbell, George S. | TIBKAT | 1953

Flight tests of a delta-wing vertically rising airplane model powered by a ducted fan

Lovell, Powell M. | TIBKAT | 1955

Preliminary experimental investigation of the flight of a person supported by a jet thrust device attached to his feet

Zimmermann, C. H. / Hill, Paul R. / Kennedy, T. L. | TIBKAT | 1953

Flight measurements of the lateral stability and control characteristics of a high-speed fighter airplane

Crane, H. L. / Beckhardt, A. R. / Matheny, C. E. | TIBKAT | 1952

Characteristics of the Nike-Cajun (CAN) rocket system and flight investigation of its performance

Royall, John F. / Garland, Benjamine J. | TIBKAT | 1957

Comparison of zero-lift drag determined by flight tests at transonic speeds of pylon, underslung, and symmetrically mounted nacelles at 40 percenmt semispan of a 45 degree sweptback wing and body combination

Hoffman, Sherwood | TIBKAT | 1951

Some considerations regarding the application of the supersonic area rule to the design of airplane fuselages

Whitcomb, Richard T. | TIBKAT | 1956

Measurements of aerodynamic heating obtained during demonstration flight tests of the Douglas D-558-II airplane

Jones, Ira P. | TIBKAT | 1952

A Simplified Method for Estimating Subsonic Lift-Curve Slope at Low Angles of Attack for Irregular Planform Wings

Spencer, Bernard, Jr. | NTRS | 1961

with a 20-step vortex method (NACA Research Memorandum L50L13) indicated good agreement for a variable-sweep configuration. ...

Civil Aviation in Communist China Since 1949

H. E. Porch | NTIS | 1968

As part of a continuing program of research on Communist China, memorandum presents the results of a study of the development of operation ...