WorldCat Identities

United States National Advisory Committee for Aeronautics

Overview
Works: 9,384 works in 11,444 publications in 1 language and 36,677 library holdings
Genres: History  Periodicals  Bibliography  Abstracts  Conference papers and proceedings  Mathematical formulae 
Roles: Other, Editor
Classifications: TL521.312, 353.00878
Publication Timeline
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Most widely held works about United States
 
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Most widely held works by United States
Orders of magnitude : a history of NACA and NASA, 1915-1980 by Frank Walter Anderson( Book )

2 editions published in 1981 in English and held by 293 WorldCat member libraries worldwide

Bibliography of aeronautics( )

in English and held by 167 WorldCat member libraries worldwide

Technical note( )

in English and held by 114 WorldCat member libraries worldwide

Technical memorandum by United States( )

in English and Undetermined and held by 107 WorldCat member libraries worldwide

Chiefly translations from foreign aeronautical journals
Report by United States( )

in English and held by 105 WorldCat member libraries worldwide

Wartime report( )

in English and held by 61 WorldCat member libraries worldwide

Aircraft circulars by United States( )

in English and held by 58 WorldCat member libraries worldwide

NACA-University conference on aerodynamics, construction, and propulsion [held at] Lewis Flight Propulsion Laboratory, Cleveland, Ohio, October 20, 21, and 22, 1954 by United States( Book )

3 editions published in 1954 in English and held by 50 WorldCat member libraries worldwide

Aeronautics in NACA and NASA( Book )

2 editions published between 1991 and 1992 in English and held by 19 WorldCat member libraries worldwide

Annual report of the National Advisory Committee for Aeronautics by United States( )

in English and held by 9 WorldCat member libraries worldwide

Square plate with clamped edges under normal pressure producing large deflections by Samuel Levy( Book )

4 editions published in 1942 in English and held by 8 WorldCat member libraries worldwide

A theoretical analysis is given for the stresses and deflections of a square plate with clamped edges under normal pressure producing large deflections. Values of the bending stress and membrane stress at the center of the plate and at the midpoint of the edge are given for center deflections up to 1.9 times the plate thickness. The shape of the deflected surface is given for low pressures and for the highest pressure considered. Convergence of the solution is considered, and it sis estimated that the possible error is less than 2 percent. The results are compared with the only previous approximate analysis known to the author and agree with 5 percent. They are also shown to compare favorably with the known exact solutions for the long rectangular plate and the circular plate
Description of stress-strain curves by three parameters by Walter Ramberg( Book )

3 editions published between 1943 and 1947 in English and held by 8 WorldCat member libraries worldwide

A simple formula is suggested for describing the stress-strain curve in terms of three parameters: namely, Young's modulus and two secant yield strengths. Dimensionless charts are derived from this formula for determining the stress-strain curve, the tangent modulus, and the reduced modulus of a material for which these three parameters are given. Comparison with the tensile and compressive data on aluminum alloy, stainless-steel, and carbon-steel sheet in NACA Technical Note No. 840 indicates that the formula is adequate for most of these materials. The formula does not describe the behavior of alclade sheet, which shows a marked change in slope at low stress. It seems probable that more than three parameters will be necessary to represent such stress-strain curves adequately
Bending of rectangular plates with large deflections by Samuel Levy( Book )

4 editions published in 1942 in English and held by 8 WorldCat member libraries worldwide

The solution of von Karman's fundamental equations for large deflections of plates is presented for the case of asimply supported rectangular plate under combined edge compression and lateral loading. Numerical solutions are given for square plates and for rectangular plates with a width-span ratio of 3:1. The effective widths according to von Karman, Bengston, Marguerre, and Cox and with experimental results by Ramberg, McPherson, and Levy. The deflections for a square plate under lateral pressure are compared with experimental and theoretical results by Kaiser. It is found that the effective widths agree closely with Marguerre's formula and with the experimentally observed values and that the deflections agree with the experimental results and with Kaiser's work
Shear lag in box beams methods of analysis and experimental investigations by Paul Kuhn( Book )

3 editions published between 1941 and 1942 in English and held by 7 WorldCat member libraries worldwide

Recommendations for numerical solution of reinforced-panel and fuselage-ring problems by Nicholas J Hoff( Book )

3 editions published between 1948 and 1949 in English and held by 6 WorldCat member libraries worldwide

The method of systematic relaxations, the matrix calculus method, and several other methods applicabel in special cases are discussed. Definite recommendations are made for obtaining the solution of reinforced-panel problems which are generally designated as shear lag problems
A unified theory of plastic buckling of columns and plates by Elbridge Z Stowell( Book )

4 editions published between 1947 and 1948 in English and held by 5 WorldCat member libraries worldwide

On the basis of modern plasticity considerations, a unified theory of plastic buckling applicable to both columns and plates has been developed. For uniform compression, the theory shows shows that long columns which bend without appreciable twisting require the tangent modulus and that long flanges which twist without appreciable bending require the secant modulus. Structures that both bend and twist when they buckle require a modulus which is a combination of the secant modulus and the tangent modulus
Critical stress of thin-walled cylinders in torsion by S. B Batdorf( Book )

5 editions published in 1947 in English and held by 5 WorldCat member libraries worldwide

A theoretical solution is given of the critical stress of thin-walled cylinders loaded in torsion. The results are presented in terms of a few simple formulas and curves which are applicable to a wide range of cylinder dimensions from very short cylinders of large radius to long cylinders of small radius. Theoretical results are found to be in somewhat better agreement with experimental results than previous theoretical work for the same range of cylinder dimensions
Principles of moment distribution applied to stability of structures composed of bars or plates by Eugene E Lundquist( Book )

4 editions published between 1943 and 1945 in English and held by 5 WorldCat member libraries worldwide

The principles of the cross method of moment distribution, which have previously been applied to the stability of structures composed of bars under axial load, are applied to the stability of structures composed of long plates under longitudinal load. A brief theoretical treatment of the subject, as applied to structures composed of either bars or plates, is included, together with an illustrative example for each of these two types of structure. An appendix presents the derivation of the formulas for the various stiffnesses and carry-over factors used in solving problems in the stability of structures composed of long plates
Effect of normal pressure on the critical shear stress of curved sheet by Norman Rafel( Book )

6 editions published between 1942 and 1945 in English and held by 3 WorldCat member libraries worldwide

Results are presented of tests of two sets of 20 curved-sheet specimens to determine the effect of normal pressure on the critical compressive and shear stress of curved sheet. It was found that normal pressure raised the critical compressive and shear stress of curved sheet except when outward bulging occurred in compression, in which case the critical stress was lowered by normal pressure
Buckling of thin-walled cylinder under axial compression and internal pressure by Hsu Lo( Book )

2 editions published in 1950 in English and held by 3 WorldCat member libraries worldwide

An investigation was made of a thin-walled cylinder under axial compression and various internal pressures to study the effect of the internal pressure on the compressive buckling stress of the cylinder. A theoretical analysis based on a large-deflection theory was also made. The theoretically predicted increase of compressive buckling stress due to internal pressure agrees fairly well with the experimental results
 
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Alternative Names

controlled identityUnited States. National Aeronautics and Space Administration

Advisory Committee for Aeronautics

Advisory Committee for Aeronautics United States

Amerika gasshukoku koku shimon iinkai

tats-Unis. Advisory Committee for Aeronautics

N.A.C.A.

NACA

NACA (National Advisory Committee for Aeronautics)

Nacionalni savetodavni komitet za aeronautiku

National advisory committee for aeronautics

National Advisory Committee for Aeronautics (.-U.)

National Advisory Committee for Aeronautics (Estados Unidos)

National Advisory Committee for Aeronautics (U.S.)

National Advisory Committee for Aeronautics United States

Nationaler Beratungsausschu fr Luftfahrt

Nationaler Beratungsausschu fr Luftfahrt United States

United States Advisory Committee for Aeronautics

United States Aeronautics, National Advisory Committee for

United States. National Advisory Committee for Aeronautics

United States Nationaler Beratungsausschu fr Luftfahrt

USA Advisory Committee for Aeronautics

USA Nationaler Beratungsausschu fr Luftfahrt

Национални саветодавни комитет за аеронаутику

Национальный консультативный комитет по воздухоплаванию

Національний консультативний комітет з повітроплавання

הוועדה הלאומית המייעצת לאווירונאוטיקה

اللجنة الاستشارية الوطنية للملاحة الجوية

کمیته رایزنی ملی هوانوردی آمریکا

தேசிய வானூர்தியியல் ஆலோசனை செயற்குழு

നാഷണൽ അഡ്വൈസറി കമ്മിറ്റി ഫോർ എയറോനോട്ടിക്സ്

アメリカ ガッシュウコク コウクウ シモン イインカイ

アメリカ航空諮問委員会

全米航空諮問委員会

美国国家航空咨询委员会

美國國家航空諮詢委員會

Languages
English (156)

Covers
Expanding the envelope : flight research at NACA and NASA