Design and fabrication of a radiative actively cooled honeycomb sandwich structural panel for a hypersonic aircraft /

Cryogenic performance of slotted brazed Rene ́41 honeycomb panels /

Hepler, Andrew K.
Swegle, Allan R.
Langley Research Center.
Boeing Aerospace Company.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1982

"June 1982"--Cover.STAR category 39."Boeing Aerospace Company."Includes bibliographical references.M...

Thermal-structural design study of an airframe-integrated scramjet : summary report /

Buchmann, O. A.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Oct. 1979."Prepared for Langley Research Center under Contract NAS1-13984."Includes bibliographical ...

Aerothermal performance of a radiatively and actively cooled panel at Mach 6.6 /

Shore, Charles P.
Weinstein, Irving.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject category 34."December 1979"--Cover.Includes bibliographical references.Mode of access: Inter...

High heat flux actively cooled honeycomb sandwich structural panel for a hypersonic aircraft /

Koch, L. C. (Leland C.)
Pagel, L. L., joint author.
Langley Research Center.
McDonnell Douglas Corporation.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1978

December 1978.Prepared for Langley Research Center under contract NAS1-12919.Mode of access: Interne...

Actively cooled plate fin sandwich structural panels for hypersonic aircraft /

Smith, L. M. (Lee Mark)
Beuyukian, C. S.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Aug. 1979."Prepared for Langley Research Center under Contract NAS1-13382."Includes bibliographical ...

Thermal design for areas of interference heating on actively cooled hypersonic aircraft /

Herring, R. L.
Stone, J. E., joint author.
McDonnell Douglas Corporation.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1978

January 1978.Prepared for Langley Research Center under contract NAS1-14140.Includes bibliographical...

Design and fabrication of a radiative actively cooled honeycomb sandwich structural panel for a hypersonic aircraft

Schaeffer, D. M.
Pagel, L. L.
Ellis, D. A.

March 1978

The panel assembly consisted of an external thermal protection system (metallic heat shields and ins...

Design and fabrication of a stringer stiffened discrete tube actively cooled panel for a hypersonic aircraft /

Anthony, Frank M.
Helenbrook, Robert G.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject category 39."February 1981."Includes bibliographical references.Mode of access: Internet

An analytical study of hydrogen cooled panels for application to hypersonic aircraft /

Flieder, W. G.
Langley Research Center.
Garrett Corporation.
United States. National Aeronautics and Space Administration.

January 1971

Prepared by The Garrett Corporation for Langley Research Center.N71-22625.Includes bibliographical r...

Actively cooled plate fin sandwich structural panels for hypersonic aircraft

Beuyukian, C. S.
Smith, L. M.

August 1979

An unshielded actively cooled structural panel was designed for application to a hypersonic aircraft...

Advanced beaded and tubular structural panels /

Musgrove, Max D. (Max Donnell)
Greene, Bruce E.
Langley Research Center.
Boeing Aerospace Company.

"Prepared by the Boeing [Aerospace] Company ... for Langley Research Center.""September 1975."Cover ...

High heat flux actively cooled honeycomb sandwich structural panel for a hypersonic aircraft

Pagel, L. L.
Koch, L. C.

December 1978

The results of a program to design and fabricate an unshielded actively cooled structural panel for ...

Elevated-temperature tests under static and aerodynamic conditions on honeycomb-core sandwich panels /

Groen, Joseph M.
Johnson, Aldie E.
United States. National Aeronautics and Space Administration.

"September 1959."Cover title.Includes bibliographical references (p. 14).Mode of access: Internet

Calculated effective thermal conductivities of honeycomb sandwich panels /

Swann, Robert T.
United States. National Aeronautics and Space Administration.

Cover title."December 1959."Heating, aerodynamic; Sandwich and laminates; Materials, properties, the...

Flightweight radiantly and actively cooled panel : thermal and structural performance /

Shore, Charles P.
Kelly, H. Neale.
Nowak, Robert J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

"October 1982"--Cover.Includes bibliographical references.Mode of access: Internet

Cryogenic performance of slotted brazed Rene ́41 honeycomb panels /

Hepler, Andrew K.
Swegle, Allan R.
Langley Research Center.
Boeing Aerospace Company.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1982

"June 1982"--Cover.STAR category 39."Boeing Aerospace Company."Includes bibliographical references.M...

Thermal-structural design study of an airframe-integrated scramjet : summary report /

Buchmann, O. A.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Oct. 1979."Prepared for Langley Research Center under Contract NAS1-13984."Includes bibliographical ...

Aerothermal performance of a radiatively and actively cooled panel at Mach 6.6 /

Shore, Charles P.
Weinstein, Irving.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject category 34."December 1979"--Cover.Includes bibliographical references.Mode of access: Inter...

High heat flux actively cooled honeycomb sandwich structural panel for a hypersonic aircraft /

Koch, L. C. (Leland C.)
Pagel, L. L., joint author.
Langley Research Center.
McDonnell Douglas Corporation.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1978

December 1978.Prepared for Langley Research Center under contract NAS1-12919.Mode of access: Interne...

Actively cooled plate fin sandwich structural panels for hypersonic aircraft /

Smith, L. M. (Lee Mark)
Beuyukian, C. S.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Aug. 1979."Prepared for Langley Research Center under Contract NAS1-13382."Includes bibliographical ...

Thermal design for areas of interference heating on actively cooled hypersonic aircraft /

Herring, R. L.
Stone, J. E., joint author.
McDonnell Douglas Corporation.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1978

January 1978.Prepared for Langley Research Center under contract NAS1-14140.Includes bibliographical...

Design and fabrication of a radiative actively cooled honeycomb sandwich structural panel for a hypersonic aircraft

Schaeffer, D. M.
Pagel, L. L.
Ellis, D. A.

March 1978

The panel assembly consisted of an external thermal protection system (metallic heat shields and ins...

Design and fabrication of a stringer stiffened discrete tube actively cooled panel for a hypersonic aircraft /

Anthony, Frank M.
Helenbrook, Robert G.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject category 39."February 1981."Includes bibliographical references.Mode of access: Internet

An analytical study of hydrogen cooled panels for application to hypersonic aircraft /

Flieder, W. G.
Langley Research Center.
Garrett Corporation.
United States. National Aeronautics and Space Administration.

January 1971

Prepared by The Garrett Corporation for Langley Research Center.N71-22625.Includes bibliographical r...

Actively cooled plate fin sandwich structural panels for hypersonic aircraft

Beuyukian, C. S.
Smith, L. M.

August 1979

An unshielded actively cooled structural panel was designed for application to a hypersonic aircraft...

Advanced beaded and tubular structural panels /

Musgrove, Max D. (Max Donnell)
Greene, Bruce E.
Langley Research Center.
Boeing Aerospace Company.

"Prepared by the Boeing [Aerospace] Company ... for Langley Research Center.""September 1975."Cover ...

High heat flux actively cooled honeycomb sandwich structural panel for a hypersonic aircraft

Pagel, L. L.
Koch, L. C.

December 1978

The results of a program to design and fabricate an unshielded actively cooled structural panel for ...

Elevated-temperature tests under static and aerodynamic conditions on honeycomb-core sandwich panels /

Groen, Joseph M.
Johnson, Aldie E.
United States. National Aeronautics and Space Administration.

"September 1959."Cover title.Includes bibliographical references (p. 14).Mode of access: Internet

Calculated effective thermal conductivities of honeycomb sandwich panels /

Swann, Robert T.
United States. National Aeronautics and Space Administration.

Cover title."December 1959."Heating, aerodynamic; Sandwich and laminates; Materials, properties, the...

Flightweight radiantly and actively cooled panel : thermal and structural performance /

Shore, Charles P.
Kelly, H. Neale.
Nowak, Robert J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

"October 1982"--Cover.Includes bibliographical references.Mode of access: Internet

Cryogenic performance of slotted brazed Rene ́41 honeycomb panels /

Hepler, Andrew K.
Swegle, Allan R.
Langley Research Center.
Boeing Aerospace Company.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1982

"June 1982"--Cover.STAR category 39."Boeing Aerospace Company."Includes bibliographical references.M...

Thermal-structural design study of an airframe-integrated scramjet : summary report /

Buchmann, O. A.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Oct. 1979."Prepared for Langley Research Center under Contract NAS1-13984."Includes bibliographical ...

Aerothermal performance of a radiatively and actively cooled panel at Mach 6.6 /

Shore, Charles P.
Weinstein, Irving.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject category 34."December 1979"--Cover.Includes bibliographical references.Mode of access: Inter...

Design and fabrication of a radiative actively cooled honeycomb sandwich structural panel for a hypersonic aircraft /

Abstract

Extracted data

Design and fabrication of a radiative actively cooled honeycomb sandwich structural panel for a hypersonic aircraft /

Abstract

Extracted data

Related items

Related items