Langley 9-inch supersonic tunnel tests of several modifications of a supersonic missile having tandem cruciform lifting surfaces : three-component data results of models having ratios of wing span to tail span less than 1 /

Comparison of lift-curve slopes for a model tested in two slotted tunnels of different sizes at high subsonic speeds /

Boswinkle, Robert W.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"June 23, 1953."Includes bibliographical references (p. 7).Mode of access: Internet

Supersonic aerodynamic characteristics of canard, tailless, and aft-tail configurations for two wing planforms /

Covell, Peter F.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 66).M...

Wind-tunnel investigation of the carry loads and mutual interference effects of 1/40-scale models of the X-15 and B-52 apirplanes in combination. /

Taylor, Robert T., NASA ressearcher
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1959

"Langley Research Center, Langley Research Center.""December 1959."Cover title.Mode of access: Inter...

Preliminary results of supersonic-jet tests of simplified wing structures /

Heldenfels, Richard R.
Rosecrans, Richard.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"July 8, 1953."Includes bibliographical references (p. 15).Mode of access: Internet

A pressure-distribution investigation of a supersonic-aircraft fuselage and calibration of the Mach number 1.40 nozzle of the Langley 4- by 4-foot supersonic tunnel /

Hasel, Lowell E.
Sinclair, Archibald R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics.

January 1950

"April 7, 1950; Declassified May 29, 1959."Includes bibliographical references (p. 14).Mode of acces...

Low subsonic flight and force investigation of a supersonic transport model with a highly swept arrow wing /

Freeman, Delma C.
Langley Research Center.

January 1967

Work performed at Langley Research Center.Includes bibliographical references (p. 19).Mode of access...

Jet effects at supersonic speeds on base and afterbody pressures of a missile model having single and multiple jets /

Charczenko, Nickolai.
Hayes, Clyde.
Langley Research Center.

Prepared at Langley Research Center."November 1963"--Cover.Includes bibliographical references (p. 8...

Mach 6 experimental and theoretical stability and performance of a cruciform missile at angles of attack up to 65⁰ /

Hartman, Edward R.
Johnston, Patrick J.
Langley Research Center.

January 1987

Prepared at Langley Research Center."July 1987"--Cover.Includes bibliographical references (p. 7-8)....

Rocket-powered flight test of a roll-stabilized supersonic missile configuration /

Gardiner, Robert A.
Zarovsky, Jacob.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1950

"January 12, 1950."Includes bibliographical references (p. 12).Mode of access: Internet

Preliminary results of the flight investigation between Mach numbers of 0.80 and 1.36 of a rocket-powered model of a supersonic airplane configuration having a tapered wing with circular-arc sections and 40©� sweepback /

D'Aiutolo, Charles T.
Mason, Homer P.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1958

"October 31, 1950. Declassified September 17, 1958."Cover title.Includes bibliographical references ...

Supersonic investigation of nozzle hinge moments of a modified Saturn C-1 model with and without jet flow /

Charczenko, Nickolai.
Lowery, Jerry L.
Langley Research Center.

Prepared at Langley Research Center."November 1963"--Cover.Includes bibliographical references (p. 9...

Supersonic longitudinal stability characteristics of the two final stages of a four-stage launch vehicle /

McKinney, Royce L.
Langley Research Center.

Prepared at Langley Research Center."March 1964"--Cover.Mode of access: Internet

Langley mach 4 scramjet test facility /

Andrews, Earl H.
Langley Research Center.

January 1985

Prepared at Langley Research Center."February 1985."Includes bibliographical references (p. 11-12).M...

Low subsonic flight and force investigation of a supersonic transport model with a double-delta wing /

Freeman, Delma C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Work performed at Langley Research Center.N68-18250.Includes bibliographical references (p. 17).Mode...

Investigation of the effects of model scale and stream Reynolds number on the aerodynamic characteristics of two rectangular wings at supersonic speeds on the Langley 9-inch supersonic tunnel /

Coletti, Donald E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"June 14, 1955."Includes bibliographical references (p. 10-11).Mode of access: Internet

Comparison of lift-curve slopes for a model tested in two slotted tunnels of different sizes at high subsonic speeds /

Boswinkle, Robert W.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"June 23, 1953."Includes bibliographical references (p. 7).Mode of access: Internet

Supersonic aerodynamic characteristics of canard, tailless, and aft-tail configurations for two wing planforms /

Covell, Peter F.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 66).M...

Wind-tunnel investigation of the carry loads and mutual interference effects of 1/40-scale models of the X-15 and B-52 apirplanes in combination. /

Taylor, Robert T., NASA ressearcher
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1959

"Langley Research Center, Langley Research Center.""December 1959."Cover title.Mode of access: Inter...

Preliminary results of supersonic-jet tests of simplified wing structures /

Heldenfels, Richard R.
Rosecrans, Richard.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"July 8, 1953."Includes bibliographical references (p. 15).Mode of access: Internet

A pressure-distribution investigation of a supersonic-aircraft fuselage and calibration of the Mach number 1.40 nozzle of the Langley 4- by 4-foot supersonic tunnel /

Hasel, Lowell E.
Sinclair, Archibald R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics.

January 1950

"April 7, 1950; Declassified May 29, 1959."Includes bibliographical references (p. 14).Mode of acces...

Low subsonic flight and force investigation of a supersonic transport model with a highly swept arrow wing /

Freeman, Delma C.
Langley Research Center.

January 1967

Work performed at Langley Research Center.Includes bibliographical references (p. 19).Mode of access...

Jet effects at supersonic speeds on base and afterbody pressures of a missile model having single and multiple jets /

Charczenko, Nickolai.
Hayes, Clyde.
Langley Research Center.

Prepared at Langley Research Center."November 1963"--Cover.Includes bibliographical references (p. 8...

Mach 6 experimental and theoretical stability and performance of a cruciform missile at angles of attack up to 65⁰ /

Hartman, Edward R.
Johnston, Patrick J.
Langley Research Center.

January 1987

Prepared at Langley Research Center."July 1987"--Cover.Includes bibliographical references (p. 7-8)....

Rocket-powered flight test of a roll-stabilized supersonic missile configuration /

Gardiner, Robert A.
Zarovsky, Jacob.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1950

"January 12, 1950."Includes bibliographical references (p. 12).Mode of access: Internet

Preliminary results of the flight investigation between Mach numbers of 0.80 and 1.36 of a rocket-powered model of a supersonic airplane configuration having a tapered wing with circular-arc sections and 40©� sweepback /

D'Aiutolo, Charles T.
Mason, Homer P.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1958

"October 31, 1950. Declassified September 17, 1958."Cover title.Includes bibliographical references ...

Supersonic investigation of nozzle hinge moments of a modified Saturn C-1 model with and without jet flow /

Charczenko, Nickolai.
Lowery, Jerry L.
Langley Research Center.

Prepared at Langley Research Center."November 1963"--Cover.Includes bibliographical references (p. 9...

Supersonic longitudinal stability characteristics of the two final stages of a four-stage launch vehicle /

McKinney, Royce L.
Langley Research Center.

Prepared at Langley Research Center."March 1964"--Cover.Mode of access: Internet

Langley mach 4 scramjet test facility /

Andrews, Earl H.
Langley Research Center.

January 1985

Prepared at Langley Research Center."February 1985."Includes bibliographical references (p. 11-12).M...

Low subsonic flight and force investigation of a supersonic transport model with a double-delta wing /

Freeman, Delma C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Work performed at Langley Research Center.N68-18250.Includes bibliographical references (p. 17).Mode...

Investigation of the effects of model scale and stream Reynolds number on the aerodynamic characteristics of two rectangular wings at supersonic speeds on the Langley 9-inch supersonic tunnel /

Coletti, Donald E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"June 14, 1955."Includes bibliographical references (p. 10-11).Mode of access: Internet

Comparison of lift-curve slopes for a model tested in two slotted tunnels of different sizes at high subsonic speeds /

Boswinkle, Robert W.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"June 23, 1953."Includes bibliographical references (p. 7).Mode of access: Internet

Supersonic aerodynamic characteristics of canard, tailless, and aft-tail configurations for two wing planforms /

Covell, Peter F.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 66).M...

Wind-tunnel investigation of the carry loads and mutual interference effects of 1/40-scale models of the X-15 and B-52 apirplanes in combination. /

Taylor, Robert T., NASA ressearcher
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1959

"Langley Research Center, Langley Research Center.""December 1959."Cover title.Mode of access: Inter...

Langley 9-inch supersonic tunnel tests of several modifications of a supersonic missile having tandem cruciform lifting surfaces : three-component data results of models having ratios of wing span to tail span less than 1 /

Abstract

Extracted data

Langley 9-inch supersonic tunnel tests of several modifications of a supersonic missile having tandem cruciform lifting surfaces : three-component data results of models having ratios of wing span to tail span less than 1 /

Abstract

Extracted data

Related items

Related items